Minimizing drag-induced forces on a wheeled vehicle

ABSTRACT

An aerodynamically optimized drag-reduction apparatus and method for optimal minimization of the drag-induced resistive forces upon a terrestrial vehicle, where the drag-induced resistive moments on wheel surfaces pivoting about the stationary point of ground contact are reduced, and the vehicle propulsive forces needed to countervail the resistive forces on the wheel are reduced. The drag reduction apparatus includes: a streamlined fairing or wind deflector positioned on a vehicle to shield the faster moving upper wheel surfaces from headwinds; an engine exhaust pipe disposed on a vehicle whereby exhaust gases deflect headwinds to shield the faster moving upper wheel surfaces of an automotive wheel; an automotive spoked wheel having streamlined oval-shaped wheel spokes; a wheel assembly with a streamlined tailfin rotatably attached to a wheel spoke; a wheel with a tapered spoke having a thin aerodynamic profile near the rim and tapering to a round profile toward the central hub; and a tire having streamlined tread blocks arranged in an aerodynamic pattern.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation of patent application Ser. No. 14/479,699, filed Sep. 8, 2014 by Garth L. Magee.

BACKGROUND Field

The present embodiment relates to vehicle wheels, and particularly to shields and devices used to reduce drag on rotating vehicle wheels.

Description of Prior Art

Inherently characteristic of rotating vehicle wheels, and particularly of spoked wheels, aerodynamic resistance, or parasitic drag, is an unwanted source of energy loss in propelling a vehicle. Parasitic drag on a wheel includes viscous drag components of form (or pressure) drag and frictional drag. Form drag on a wheel generally arises from the circular profile of a wheel moving though air at the velocity of the vehicle. The displacement of air around a moving object creates a difference in pressure between the forward and trailing surfaces, resulting in a drag force that is highly dependent on the relative wind speed acting thereon. Streamlining the wheel surfaces can reduce the pressure differential, reducing form drag.

Frictional drag forces also depend on the speed of wind impinging exposed surfaces, and arise from the contact of air moving over surfaces. Both of these types of drag forces arise generally in proportion to the square of the relative wind speed, per the drag equation. Streamlined design profiles are generally employed to reduce both of these components of drag force.

The unique geometry of a wheel used on a vehicle includes motion both in translation and in rotation; the entire circular outline of the wheel translates at the vehicle speed, and the wheel rotates about the axle at a rate consistent with the vehicle speed. Form drag forces arising from the moving outline are apparent, as the translational motion of the wheel rim must displace air immediately in front of the wheel (and replace air immediately behind it). These form drag forces arising across the entire vertical profile of the wheel are therefore generally related to the velocity of the vehicle.

As the forward profile of a wheel facing the direction of vehicle motion is generally symmetric in shape, and as the circular outline of a wheel rim moves forward at the speed of the vehicle, these form drag forces are often considered uniformly distributed across the entire forward facing profile of a moving wheel (although streamlined cycle rims can affect this distribution somewhat). This uniform distribution of pressure force is generally considered centered on the forward vertical wheel profile, and thereby in direct opposition to the propulsive force applied at the axle, as illustrated in FIG. 24.

However, as will be shown, frictional drag forces are not uniformly distributed with elevation on the wheel, as they are not uniformly related to the speed of the moving outline of the wheel rim. Instead, frictional drag forces on the wheel surfaces are highly variable and depend on their elevation above the ground. Frictional drag must be considered separate from form drag forces, and can be more significant sources of overall drag on the wheel and, as will be shown, thereby on the vehicle.

The motion of wheel spokes through air creates considerable drag, especially at higher relative wind speeds. This energy loss is particularly critical in both bicycle locomotion and in high-speed vehicle locomotion. Previous efforts to reduce this energy loss in bicycle wheels have included bladed-spoke designs; the addition of various coverings attached directly to the wheel; and the use of deeper, stiffer, and heavier aerodynamic rims. As winds, and particularly headwinds, are a principal source of energy loss in bicycle locomotion, expensive aerodynamic wheel designs have become increasingly popular. However, these aerodynamic wheel designs have often been tuned to reduce form drag, rather than frictional drag. As a result, augmented frictional drag forces present on these larger-surfaced aerodynamic wheel designs tend to offset much of the gains from reduced form drag forces, thereby negating potential reductions in overall drag.

Bladed spokes, tapered in the direction of motion through the wind, are designed to reduce form drag. These streamlined spokes suffer from increased design complexity, increased weight and higher costs. In addition, such bladed designs are more susceptible to crosswind drag effects: The increased surface area of the bladed spoke can rapidly increase form drag in the presence of any crosswind; any crosswind directed upon the flat portion of the spoke quickly increases pressure drag upon the spoke.

Under low crosswinds, the bladed spoke presents a relatively small forward profile facing oncoming headwinds, minimizing form drag. Indeed, the thin profile of the blade generally minimizes form drag over that of round spoke profile. However, most external winds will not be precisely aligned co-directional with the forward motion of the wheel. Such winds cause a crosswind component to be exerted upon the wheel, leading to flow-separation—and thus turbulence—behind the bladed spoke, and thereby generally negate the potential aerodynamic benefit of the bladed-spoke design. Under high crosswinds, the round spoke profile may even outperform the bladed spoke in terms of drag reduction. Perhaps a result of these conflicting factors, the bladed spoke has not become the common standard for use in all bicycle competitions.

Wheel covers generally include a smooth covering material attached directly to the wheel over the outside of the spokes, generally covering a large portion of the wheel assembly, often extending from the wheel rim to the axle. Wheel covers add weight to the wheel assembly and can result in more wheel surface area being exposed to winds. The additional weight on the wheel is detrimental to wheel acceleration, while the large surface area of the cover can increase frictional drag. Although covering the wheel spokes can reduce form drag forces thereon, the increased frictional drag forces on the larger surface areas can largely offset any aerodynamic benefit. In addition, covering large portions of the wheel also increases bicycle susceptibility to crosswind forces, destabilizing the rider. For this reason, wheel covers are generally used only on the rear wheel of a bicycle, and generally only under low crosswind conditions. Perhaps as a result of these conflicting factors, wheel covers have not become the standard equipment for use in all bicycle competitions.

Recently developed for use on bicycles, deeper, stiffer and heavier aerodynamic wheel rims suffer several drawbacks: deeper (wider along the radial direction of the wheel) and streamlined rims are often used to reduce profile drag on high-performance bicycle wheels. As mentioned, these rims are generally designed to reduce profile drag under various crosswind conditions. However, these deeper rims—having generally larger rotating surface areas—can dramatically increase friction drag. As will be shown, friction drag is particularly increased on the expanded upper wheel surfaces, largely negating any potential benefit of the reduced profile drag. In addition, such deep wheel rims with minimal spokes must be made stronger and stiffer—typically with double-wall construction—than conventional single-wall, thin-rim designs. As a result, such deep rims often ride more harshly over bumpy terrain, and are generally heavier, adding weight to the bicycle, which becomes a drawback when the grade becomes even slightly uphill.

As a result of these and other countervailing factors, no single wheel design has emerged as the preferred choice for reducing drag on bicycle wheels over a wide range of operating conditions. Instead, a variety of wheel designs are often employed in modern racing bicycles. In the same competition, for example, some riders may choose to use bladed spokes, while others choose round spokes, while still others choose deep rims or wheel covers. The differences in performance between these various wheel designs appear to only marginal affect the outcome of most races.

In sports cars, wheel covers have been employed to reduce aerodynamic vortices from developing inside the inner wheel assembly. These covers smooth the air flowing over the outer wheel and deflect a portion of the air to the brake linings, providing cooling thereon. In addition, various wings attached to the body of the car have been employed to deflect air around the drag-inducing exposed wheels. Such wings are generally located low to the ground, and are often configured to deflect air to one side or the other of exposed wheels, or to provide vehicle down-forces to counteract significant lifting forces generated by the exposed wheels. As will be shown, use of these wings to deflect air upwards onto the upper wheel can actually augment the down force problem, as well as contribute to more overall vehicle drag. And related flip-up deflectors have been incorporated into the body molding of some sports cars, although these have been generally limited to placement in front of the semi-exposed rearmost wheel. Such flip-up deflectors have also been used to augment down-forces in order to enhance vehicle stability at high speeds.

In various cycles, fenders and mud-covers have been used to cover wheels for other purposes. However, these items are generally oriented on the cycle consistent with their intended purpose of shielding the rider from debris ejected from the wheel. As such, they are not necessarily designed to be either forwardly positioned, nor closely fitted to the tire and wheel for aerodynamic shielding purposes. On some bicycles, skirt guards have been employed specifically to prevent clothing of the rider from becoming entangled with the rotating wheel. However, these guards are often made of porous construction, and are generally employed on the rear-most wheel, rather than on the front-most wheel, where the potential aerodynamic benefit is generally greater.

Perhaps because aerodynamic devices are generally not allowed by rules governing many bicycle competitions, development of fairings for bicycles remains somewhat limited. Instead, fairings have been generally used to cover either the entire cycle, or the broad front area of the cycle, shielding both rider and cycle. Enclosing-type fairings typically have quite large surface areas, which augment frictional drag forces, largely negating any benefit in reducing form drag from streamlining the forward profile of the bicycle. Nevertheless, numerous bicycle speed records have been achieved using these larger fairings, validating their effectiveness. Frontal wind-deflecting fairings are typically used to reduce form drag on various components on a cycle; however, their greatly expanded surface areas can minimize their effectiveness by introducing greater frictional drag. The potential effectiveness of using smaller fairings—having minimal form and friction drag—for shielding specific, critical, drag-sensitive areas of moving wheel surfaces has not been properly recognized.

A study by Sunter and Sayers (2001), Aerodynamic Drag Mountain Bike Tyres, Sports Engineering, 4, 63-73, proposed and tested the use of a front-mounted wind-deflector fender for relatively low-speed, rough-surfaced, down-hill racing mountain bicycle front wheels. However, as will be shown, the tested fender was unnecessarily extensive; its extended design—covering the tire to well below the level of the axle—failed to focus properly on key sources of drag on a typical bicycle wheel. Instead, in this investigation, variations in drag were measured with differing tire tread patterns, and differing fender clearances, using knobby mountain bike tires, and were measured on the front wheel only. Moreover, sufficient fender clearances with the tire were investigated, with the aim of determining any potential benefit in reducing drag on the bicycle against the potential mud accumulation there-between.

Referencing an earlier study, Kyle (1985) Aerodynamic Wheels. Bicycling, December, 121-124, in this later study, Sunter and Sayers noted a 30% increase in drag on a wheel rotating with a speed equivalent to the exposed headwind, versus a stationary wheel exposed to the same headwind. As reported, this measurement seems to have represented the increase in torque needed to rotate the wheel about the axle. However, the change in torque measured about the axle on a fixed wheel mounted in an air-stream—as will be shown—cannot be considered an accurate representation of the change in drag force required to propel the bicycle. Torque measured this way is only an indirect factor needed to determine the effects on overall bicycle drag. As will be shown, the net drag force is generally not well centered on the rotating bicycle wheel, causing drag forces on the upper wheel to be magnified. Indeed, the offset drag force on the wheel contributes significantly more to overall bicycle drag than commonly understood.

A number of studies of bicycle wheel drag measured in wind tunnels also fail recognize the importance of drag forces on the upper wheel. Tests are typically conducted with the wheel suspended in the airstream, with the drag on the wheel measured via force gauges attached to the suspension arm. As will be shown, the magnification of upper wheel drag forces occurs when the wheel is in contact with the ground. Measuring drag on wheels suspended in an airstream will yield incomplete results, particularly for application to moving vehicles.

For example, an earlier study by Greenwell et al, Aerodynamic characteristics of low-drag bicycle wheels, Aeronautical Journal, 1995, 99, 109-120, measured translational drag on a wheel suspended from a torsion tube in a wind tunnel, where the wheel was driven by a motor and made no contact with a ground plane. They concluded that in this configuration—unexpectedly—rotational speed had little influence on the translational drag force directed upon the wheel assembly.

In a more recent study, Moore and Bloomfield, Translational and rotational aerodynamic drag of composite construction bicycle wheels, Proceedings of the Institution of Mechanical Engineers, Part P: Journal of Sports Engineering and Technology Jun. 1, 2008, vol. 222, no. 2, 91-102, the measured drag was extended to include rotational drag on the wheel. However, this study also failed to include a ground plane in contact with the wheel; the wheel remained suspended wind tunnel. As mentioned, this configuration does not accurately reflect the total retarding force upon a vehicle in motion caused by drag forces on the wheel.

Sunter and Sayers also failed to recognize the magnifying effect that an off-center net drag force on the wheel can have on overall bicycle drag. Instead, they concluded that with the modest improvement in drag torque measured upon the rotating wheel using the wind-deflecting fender, only corresponding modest improvement in overall bicycle drag could be expected. They further concluded that the use of extensive front-wheel wind-deflecting fenders—having a rather large forward profiles—might thus prove beneficial in the specific application of mountain bicycle downhill racing, where only modest reductions in overall drag might yield a winning advantage in higher speed races. This conclusion would be consistent with the faulty observation that total drag forces are generally well centered on the wheel.

It has long been recognized that minimizing drag on large trucks and their trailers has significant potential for improving fuel economies. Extensive wind deflectors have been used in front of the rear wheels on extended truck trailers, but are generally designed to deflect very large volumes of air to the either side of the rear wheels. Deflecting unnecessary volumes of air with large fairings, can produce significant form drag by the fairing itself, thereby negating much of the intended benefit in reducing wheel drag. And as will be shown, deflecting air below the level of the axle can be particularly detrimental in reducing overall vehicle drag.

For example, in patent US 2010/0327625A1, a V-shaped air deflector is shown positioned in front of a wheel for the purpose of deflecting large volumes of air to either side in order to reduce wheel drag. However, the deflector shown is unnecessarily large, introducing substantial form drag. And the deflector is positioned centered at the elevation of the axle, extending symmetrically above and below the axle. As mentioned, deflecting air onto lower surfaces of the wheel can be detrimental to reducing overall drag on the vehicle. And as shown, the deflector fails to fully shield the most critical drag-inducing uppermost surfaces of the wheel.

In U.S. Pat. No. 6,974,178B2, the deflectors shown are simply unnecessarily large, again introducing substantial form drag.

Other examples in the art also deflect air downward onto the lower surfaces of the wheel, thereby negating much of the intended aerodynamic benefit. These include trailer wheel deflectors of patents US 2010/0066123A1, U.S. Pat. No. 4,640,541, U.S. Pat. No. 4,486,046 and U.S. Pat. No. 4,262,953.

Other examples in the art also shield headwinds from lower surfaces of the wheel below the axle, thereby also negating much of the intended aerodynamic benefit. These include fairings of patents US 2011/0080019A1, U.S. Pat. No. 7,520,534B2, U.S. Pat. No. 7,322,592B2, U.S. Des. 377,158, U.S. Pat. No. 5,348,328, U.S. Pat. No. 4,773,663, U.S. Pat. No. 4,411,443, U.S. Pat. No. 4,326,728 and U.S. Pat. No. 2,460,349.

Wheel fairings often used on light aircraft are generally designed for reduced form drag of the wheel assembly while airborne, and generally cover the upper wheel to well below the axle. An example is shown in U.S. Pat. No. 4,027,836. Wheel pants designed as mud covers for shielding wings from ejected debris are also seen in the art, showing an upper wheel fender designed with extensive streamlined surfaces often extending substantially above and behind the wheel. As will be shown, such designs are not optimized for terrestrial use, either by extending below the level of the axle, or by not optimally shielding the most critical drag-inducing surfaces of the upper wheel.

Other examples in the art show skirt guards on the rear wheel of cycles, where the potential aerodynamic benefit is considerably less than that of the front wheel. These include guards of patents U.S. D634,2495, U.S. Pat. No. 3,101,163 and U.S. Pat. No. 1,027,806. And fender of patent U.S. D612,781S is not shown mounted on a vehicle.

Spoke art includes many examples having rectangular or otherwise non-aerodynamic cross-sectional profiles of wheel spokes for use in automotive applications. Examples include patents U.S. D460,942, U.S. D451,877, U.S. D673,494, U.S. D396,441 and others.

Cycle spoke art includes a tapered spoke of U.S. Pat. No. 5,779,323 where the cross-sectional profile of the spoke changes from more highly elliptical near the wheel hub to more generally oval near the wheel rim. As will be shown, the spoke shown is tapered to minimize—rather than maximize—any aerodynamic benefit, especially when used in the presence of crosswinds.

Tires are generally designed with tread patterns intended to maximize traction with the road surface and to minimize rolling friction and road noise. A wide variety of tread patterns exist, each designed for specific vehicle applications. Some tires with aggressive tread patterns are designed for maximum traction in off-road conditions. These tires generally have square or rectangular lugged patterns in the tread, and suffer from increased road noise and wind resistance. The need for tires with aggressive tread patterns specifically designed to reduce drag on the vehicle have been largely overlooked.

For example, in US patent 2007/0151644 A1, an oval-shaped tread pattern is shown. While oval shaped tread lugs have the potential to reduce drag, their closely spaced pattern shown diverts most of the air to flow over the top surfaces of the tire, rather than between the lugs. Moreover, the closely spaced oval lugs are designed to reduce stresses during tire compression—thereby improving the rolling resistance of the tire—and to reduce the incidence of trapping stones between the lugs. As such, the minimally spaced lugs are an essential characteristic of this embodiment. As disclosed, any minor improvement in the aerodynamic characteristics of the tire was not included.

SUMMARY

An embodiment comprises an aerodynamically optimized wheel cover shielding critical upper drag-inducing wheel surfaces from headwinds, thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises an aerodynamically optimized wind-deflecting fairing shielding critical upper drag-inducing wheel surfaces from headwinds, thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises a vehicle engine exhaust pipe disposed to cause ejected exhaust gases to deflect headwinds to shield critical upper drag-inducing wheel surfaces, thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises an automotive spoked wheel having streamlined oval-shaped wheel spokes, arranged in one or more transverse rows for enhanced axial strength, thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises a streamlined tailfin rotatably attached to a wheel spoke, able to pivot about the spoke in response to varying crosswind conditions, thereby reducing potential turbulent flow separation behind the spoke and tailfin due to crosswinds, and thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises a cycle wheel spoke tapered from a streamlined blade or highly elliptical cross-sectional profile nearest the wheel rim for reduced drag from higher speed headwinds, to a more circular cross-sectional profile nearest the wheel central hub where the relative crosswind components are higher, thereby minimizing potential drag-induced turbulent flow separation behind spoke surfaces along the entire length of the spoke, and thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises tire having aerodynamically optimized tread blocks disposed in an aerodynamically optimized pattern, reducing drag from headwinds on critical upper drag-inducing tire surfaces, and thereby reducing the total drag-induced resistive forces upon the wheel assembly and minimizing needed vehicle propulsive counter-forces.

An embodiment comprises a method for optimally minimizing the total drag-induced resistive forces upon the wheel assembly of a vehicle, and thereby minimizing needed vehicle propulsive counter-forces.

DESCRIPTION OF THE DRAWINGS

While one or more aspects pertain to most wheeled vehicles not otherwise having fully shielded wheels that are completely protected from oncoming headwinds, the embodiments can be best understood by referring to the following figures.

FIG. 1 is a front cycle wheel assembly, as typically found on a bicycle or motorcycle, where a fairing is attached and positioned as shown to each interior side of the fork assembly, thereby shielding the upper- and front-most surfaces of the spoked wheel from oncoming headwinds.

FIG. 2 is a front cycle wheel assembly, as typically found on a bicycle or motorcycle, where a fender is attached and positioned as shown to the fork assembly, thereby shielding the upper- and front-most surfaces of the tire and wheel rim from oncoming headwinds.

FIG. 3 is a front cycle wheel assembly, as typically found on a bicycle or motorcycle, where a combination fender and fairing assembly is attached and positioned as shown to the fork assembly, thereby shielding the upper- and front-most surfaces of the tire, wheel rim and spoked inner-wheel structure from oncoming headwinds.

FIG. 4 is a vehicle wheel assembly, as typically found on a sports car, where a fender is attached and positioned as shown to the wheel suspension assembly, thereby shielding the upper- and front-most surfaces of the tire from oncoming headwinds.

FIG. 5 is a vehicle wheel assembly, as typically found on a sports car, where a fender and fairing assembly is attached and positioned as shown to the wheel suspension assembly, thereby shielding both the upper- and front-most surfaces of the tire, and the upper inner-wheel structure from oncoming headwinds.

FIG. 6 is a vehicle wheel assembly, as typically found on a sports car, where a fairing assembly is attached either to the wheel suspension assembly or to the car body structure, and positioned as shown, deflecting upward any wind impinging thereon, and thereby shielding both the upper- and front-most surfaces of the tire from oncoming headwinds.

FIG. 7 is a front cycle wheel assembly, as typically found on a bicycle or motorcycle, where a fairing is attached and positioned as shown to each side of the fork assembly, and where said fairing includes a movable lower section, which may be adjusted to expand or collapse the total surface area of the fairing to accommodate a range of crosswind conditions.

FIG. 8 shows an example of prior art for automotive spoked wheels with minimal spokes, as typically found on modern automobiles, illustrating the typical square profile of the spokes, which increases drag on critical rotating wheel surfaces.

FIG. 9 shows an example of prior art for automotive spoked wheels with many outwardly-positioned spokes, as typically found on high-performance sports cars, illustrating the typical rectangular profile of the spokes, which increases drag on critical rotating wheel surfaces.

FIG. 10 shows the drag-inducing, rectangular cross-sectional profile typical of prior-art spokes used in automotive wheels, as illustrated in FIGS. 8 and 9.

FIG. 11 shows the streamlined, drag-reducing, oval-shaped cross-sectional profile of a spoke to be used in one or more of the embodiments, including automotive wheels.

FIG. 12 shows an automotive wheel with these streamlined, drag-reducing, oval cross-sectional shaped spokes, thereby reducing drag on critical rotating wheel surfaces.

FIG. 13 shows an automotive wheel with these streamlined, drag-reducing, oval cross-sectional shaped spokes, thereby reducing drag on critical rotating wheel surfaces. Two rows of spokes are shown, slightly offset axially from each other, thereby increasing the strength of the wheel in the transverse direction.

FIG. 14 shows the tapered, drag-reducing cross-sectional profile of a spoke tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates.

FIG. 15 shows a short section of the tapered, drag-reducing tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates.

FIG. 16 shows several spoke tailfins installed on a typical round wire spoke, where each spoke tailfin is free to swivel about the spoke independently, and thereby to adjust to varying crosswind influences as the wheel rotates.

FIG. 17 shows a plot of calculated average moments—about the ground contact point—of drag force, that are exerted upon rotating wheel surfaces as a function of the elevation above the ground. The relative drag forces are determined from calculated wind vectors for the rotating surfaces on a wheel moving at a constant speed of V, and plotted for several different wind and wheel-surface shielding conditions. Specifically, relative magnitudes in average drag moments about the ground contact point as a function of elevation are plotted, for eight conditions: comparing with (dashed lines) and without (solid lines) shielding covering the upper third of wheel surfaces, for tailwinds equal to half the vehicle speed; for null headwinds; for headwinds equal to half the vehicle speed; and for headwinds equal to the vehicle speed. The rising solid curves plotted show the highest moments to be near the top of the wheel, while the dashed curves show the effect of the upper shield in substantially reducing the average drag moments on the rotating wheel.

FIG. 18 shows a plot of calculated relative drag torque exerted upon rotating wheel surfaces as a function of elevation above the ground. The relative total drag torques are determined from the calculated average moments in combination with the chord length at various elevations on a wheel moving at a constant speed of V, for several different wind and wheel-surface shielding conditions. Relative magnitudes in total drag torque about the ground contact point as a function of elevation are plotted for eight conditions: comparing with (dashed lines) and without (solid lines) shielding covering the upper third of wheel surfaces, for tailwinds equal to half the vehicle speed; for null headwinds; for headwinds equal to half the vehicle speed; and for headwinds equal to the vehicle speed. The areas under the plotted curves represent the total torque from frictional drag on wheel surfaces. Comparing the differences in area under the plotted curves reveals the general trend of the upper shield to substantially reduce the total drag torque on the rotating wheel.

FIG. 19 shows a tapered spoke for use on a typical racing bicycle wheel. The spoke is shown tapering from a highly elliptical cross-sectional profile located nearest the wheel rim—shown at the top of the figure—to a more circular cross-sectional profile located on the spoke nearest the wheel central hub—shown at the bottom of the figure.

FIG. 20 shows a side view of the tapered spoke of FIG. 19.

FIG. 21 shows the highly elliptical cross section A-A of the tapered spoke shown in FIGS. 19 and 20.

FIG. 22 shows the more oval cross section B-B of the tapered spoke shown in FIGS. 19 and 20.

FIG. 23 shows the near circular cross section C-C of the tapered spoke shown in FIGS. 19 and 20.

FIG. 24 is a diagram of a wheel rolling on the ground representing typical prior art models, showing the net pressure drag force (P) exerted upon the forward wheel vertical profile—which moves at the speed of the vehicle—being generally centered near the axle of the wheel and balanced against the propulsive force (A) applied at the axle.

FIG. 25 is a diagram of a wheel rolling on the ground, showing the net friction drag force (F) upon the wheel surfaces—which move at different speeds depending on the elevation from the ground—being offset from the axle and generally centered near the top of the wheel. A ground reaction force (R)—arising due to the drag force being offset near the top of the wheel—is also shown. The force (A) applied at the axle needed to overcome the combination of drag forces (F+P) and reaction force (R) is also shown.

FIG. 26 shows a tire with an off-road tread pattern typical of prior art, having relatively sharp, angular, non-aerodynamic both windward- and leeward-facing sides on each tread block.

FIG. 27 shows an aerodynamic tread pattern with aggressive tread blocks having relatively sharp, angular, non-aerodynamic windward-facing sides for traction, and more smooth and streamlined leeward-facing sides for minimizing drag. The tread blocks are shown separated and offset longitudinally in order to partially redirect air flowing from the front leading surface of one block toward the rear trailing surface of an adjacent block, thereby reducing pressure drag on the adjacent block.

FIG. 28 shows an aerodynamic tread pattern with aggressive tread blocks having relatively sharp, angular, non-aerodynamic windward-facing sides for traction, and more smooth and streamlined leeward-facing sides for minimizing drag. The tread blocks are show separated and offset longitudinally in an oblique arrangement, in order to partially redirect air flowing from the front leading surface of one block toward the rear trailing surface of an adjacent block—thereby reducing pressure drag on the adjacent block—and toward the outside of the tire.

FIG. 29 shows an aerodynamic tread pattern with aggressive tread blocks having oval-shaped tread blocks oriented with wider sides positioned laterally for more traction, while having a substantially streamlined profiles for minimizing drag. Such a symmetrical tread pattern allows for bi-directional mounting on a vehicle. The tread blocks are shown separated and offset sufficiently in order to partially redirect air flowing from the front leading surface of one block toward the rear trailing surface of an adjacent block, thereby reducing pressure drag on the adjacent block.

FIG. 30 shows an aerodynamic tread pattern with aggressive tread blocks having oval-shaped tread blocks oriented with wider sides positioned longitudinally for more drag reduction, and having a substantially streamlined profiles for minimizing drag. Such a symmetrical tread pattern allows for bi-directional mounting on a vehicle. The tread blocks are shown separated and offset sufficiently in order to partially redirect air flowing from the front leading surface of one block toward the rear trailing surface of an adjacent block, thereby reducing pressure drag on the adjacent block.

FIG. 31 shows prior art of a typical top-fuel dragster race-car having engine exhaust pipes arranged in a linear array to direct exhaust gases substantially to the outside of the rear wheel assembly.

FIG. 32 shows a typical top-fuel dragster race-car having engine exhaust pipes arranged in a distributed array to direct exhaust gases directly above the rear wheel assembly, spanning the zone shielding the entire width of the upper surfaces of the wide tire.

FIG. 33 shows a cross section of one-half of an automotive wheel assembly having nonparallel rows of aerodynamic spokes for strengthening the wheel in the axial direction.

FIG. 34 shows a tapered spoke for use on a typical racing bicycle wheel. The spoke is shown tapering from a highly elliptical cross-sectional profile located nearest the wheel rim—shown at the top of the figure—to a more circular cross-sectional profile located on the spoke approximately midway toward the wheel central hub—shown at the bottom of the figure. The circular profile continues from the midway location toward the central hub.

FIG. 35 shows a side view of the tapered spoke of FIG. 34.

FIG. 36 shows the highly elliptical cross section AA-AA of the tapered spoke shown in FIGS. 34 and 35.

FIG. 37 shows the more oval cross section BB-BB of the tapered spoke shown in FIGS. 34 and 35.

FIG. 38 shows the near circular cross sections CC-CC and DD-DD of the tapered spoke shown in FIGS. 34 and 35.

FIG. 39 shows the drag-reducing cross-sectional profile of a longitudinally-tapered spoke tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates.

FIG. 40 shows the tapered, drag-reducing cross-sectional profile of a spoke tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates. The tailfin is also tapered from a longer width end positioned closer to the wheel rim, toward a shorter width end positioned closer to the wheel hub.

FIG. 41 shows a short section of the longitudinally-tapered, drag-reducing tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates.

FIG. 42 shows a longer section of the longitudinally-tapered, drag-reducing tailfin installed on a typical round wire spoke, where the spoke tailfin is free to swivel about the spoke and thereby to adjust to varying crosswind influences as the wheel rotates.

DETAILED DESCRIPTION

Various embodiments are described below in detail, each with means providing a reduction in drag on the wheel assembly of a vehicle. As such, each may considered as one embodiment of a comprehensive category of embodiments, whose scope is limited to that defined herein, and later referred thereto as: drag reduction means.

Furthermore, embodiments depicted in FIGS. 1, 2, 3, 4, 5 and 7 are described below and belong to a comprehensive category of embodiments, whose scope is limited to that defined herein, and later referred thereto as: wheel cover.

First Embodiment Description FIG. 1

As shown in FIG. 1, a streamlined fairing 1 is attached to the inside of a front fork tube assembly 2 of a typical bicycle 3 having spoked wheels 4. The fairing 1 is positioned closely adjacent to the inside structure of wheel 4, covering much of the upper and front-most quadrant of the wheel 4 as shown, and is rigidly fixed to front-fork tube assembly 2 using fastener 11 and strut 10. While only one fairing 1 is shown, the embodiment will generally include a similar fairing 1 located on the opposite side of the wheel 4, thereby shielding the entire upper inner structure of wheel 4 from the oncoming wind caused by forward motion of cycle 3. The fairing 1 has sufficient structural rigidity to allow close placement to spokes 5 and rim 6 of the wheel 4, thereby minimizing oncoming wind from leaking into the inner structure of wheel 4.

With fairing 1 configured in this way, the spokes 5 positioned near the top of the wheel 4 are shielded from headwinds. Shielded in this way, the topmost spokes 5 are moving at an effective wind speed generally less than or equal to the ground speed of the cycle 3, rather than moving at an effective headwind speed of up to nearly twice the ground speed of cycle 3. As a result, the aerodynamic drag forces exerted upon the topmost spokes 5 are greatly reduced.

The reduction in drag force due to fairing 1 is generally greater near the top of the wheel 4, where the spokes 5 are moving fastest with respect to headwinds otherwise impinging thereupon. As uppermost spokes 5 rotate away from the topmost point to an intermediate position with respect to either of the two lateral mid-points at the height of the axle on the wheel 4, these headwind drag forces are greatly reduced.

The embodiment shown in FIG. 1 includes a minimal fairing 1 positioned closely adjacent to the wheel, and shielding generally the most critical upper and forward-oriented quadrant of wheel 4, minimizing the addition of unnecessary weight or drag-inducing structure to cycle 3. The fairing 1 shown extends sufficiently rearward to provide a measure of profile shielding of the rear portion of the wheel and spokes, diverting the wind from impinging directly the rear rim of the wheel, and thereby permitting a generally streamlined flow to be maintained across the entire upper section of wheel assembly.

First Embodiment Operation FIGS. 1, 17, 18, 23 and 24

The shielding provided by fairing 1 is particularly effective since aerodynamic forces exerted upon exposed vehicle surfaces are generally proportional to the square of the effective wind speed impinging thereon. Moreover, the power required to overcome these drag forces is generally proportional to the cube of the effective wind speed. Thus, it can be shown that the additional power required to overcome these drag forces in propelling a vehicle twice as fast over a fixed distance, in half the time, increases by a factor of eight. And since this power requirement is analogous to rider effort—in the case of a bicycle rider—it becomes critical to shield the most critical drag-inducing surfaces on a vehicle from oncoming headwinds.

In any wheel used on a vehicle, and in the absence of any external headwinds, the effective horizontal wind speed at a point on the wheel at the height of the axle is equal to the ground speed of the vehicle. Indeed, the effective headwind speed upon any point of the rotating wheel depends on that point's current position with respect to the direction of motion of the vehicle.

Notably, a point on the moving wheel coming into direct contact with the ground is necessarily momentarily stationary, and therefore is not exposed to any relative wind speed, regardless of the speed of the vehicle. While the ground contact point can be rotating, it is not translating; the contact point is effectively stationary. And points on the wheel nearest the ground contact point are translating with only minimal forward speed. Hence, drag upon the surfaces of the wheel nearest the ground is generally negligible.

Contrarily, the topmost point of the wheel assembly (opposite the ground) is exposed to the highest relative wind speeds: generally at least twice that of the vehicle speed. And points nearest the top of the wheel are translating with forward speeds substantially exceeding the vehicle speed. Thus, drag upon the surfaces of the upper wheel can be quite substantial. Lower points on the wheel are exposed to lesser effective wind speeds, approaching a null effective wind speed—and thus negligible drag—for points nearest the ground.

Importantly, due to the rotating geometry of the wheel, it can be shown that the effective combined frictional drag force exerted upon the wheel is typically centered in closer proximity to the top of the wheel, rather than centered closer to the axle as has been commonly assumed in many past analyses of total wheel drag forces. While the net pressure (or form) drag (P) force on the forwardly facing profile of the wheel is generally centered with elevation and directed near the axle on the wheel (as shown in FIG. 24), the net frictional drag force (F) upon the moving surfaces is generally offset to near the top of the wheel (as shown in FIG. 25).

Indeed, it is near the top of the wheel where the relative winds are both greatest in magnitude, and are generally oriented most directly opposed to the forward motion of rotating wheel surfaces. Moreover, in the absence of substantial external headwinds, the frictional drag exerted upon the lower wheel surfaces contributes relatively little to the net drag upon the wheel, especially when compared to the drag upon the upper surfaces. The combined horizontal drag forces (from pressure drag from headwinds deflected by both the leading and trailing wheel forwardly facing profiles, and from frictional drag from headwinds impinging upon the forwardly moving surfaces) are thus generally concentrated near the top of the wheel under typical operating conditions. Moreover, with the faster relative winds being directed against the uppermost wheel surfaces, total drag forces combine near the top to exert considerable retarding torque upon the wheel.

As mentioned, the horizontal drag forces are primarily due to both pressure drag forces generally distributed symmetrically across the forwardly facing vertical profiles of the wheel, and to winds in frictional contact with moving surfaces of the wheel. Pressure drag forces arise primarily from the displacement of air from around the advancing vertical profile of the wheel, whose circular outline moves at the speed at the vehicle. As discussed above, since the entire circular profile moves uniformly at the vehicle speed, the displacement of air from around the moving circular profile is generally uniformly distributed with elevation across the forwardly facing vertical profile of the wheel. Thus, these pressure drag forces (P, as shown in FIG. 24 and FIG. 25) are also generally evenly distributed with elevation across the entire forwardly facing vertical profile of the wheel, and centered near the axle. And these evenly distributed pressure drag forces arise generally in proportion only to the effective headwind speed of the vehicle.

Frictional drag forces (F, as shown FIG. 25), however, are concentrated near the top of the wheel where moving surfaces generally exceed vehicle speed—while the lower wheel surfaces move at less than the vehicle speed. Since drag forces are generally proportional to the square of the effective wind speed, it becomes apparent that with increasing wind speed, that these upper wheel frictional drag forces directed upon the moving surfaces increase much more rapidly than do pressure drag forces directed upon the forward profile of the wheel. Indeed, these friction drag forces generally arise in much greater proportion to an increasing effective headwind speed of the vehicle. Nevertheless, these increased frictional drag forces being directed on the upper wheel is only a partial factor contributing to augmented wheel drag forces being responsible for significantly retarded vehicle motion.

Significantly, both types of drag forces can be shown to exert moments of force pivoting about the point of ground contact. And as such, either type of drag force exerted upon the upper wheel retards vehicle motion considerably more than a similar force exerted upon a substantially lower surface of the wheel. Minimizing these upper wheel drag forces is therefore critical to improving propulsive efficiency of the vehicle.

Also important—and due to the rotating geometry of the wheel—it can be shown that the vehicle propulsive force on the wheel applied horizontally at the axle must substantially exceed the net opposing drag force exerted near the top of the wheel. These forces on a wheel are actually leveraged against each other, both pivoting about the same point—the point on the wheel which is in stationary contact with the ground—and which is constantly changing lateral position with wheel rotation. Indeed, with the geometry of a rolling wheel momentarily pivoting about the stationary point of ground contact, the lateral drag and propulsive forces each exert opposing moments of force on the wheel centered about this same point in contact with the ground.

Furthermore, unless the wheel is accelerating, the net torque from these combined moments on the wheel must be null: The propulsive moment generated on the wheel from the applied force at the axle must substantially equal the opposing moment from drag forces centered near the top of the wheel (absent other resistive forces, such as bearing friction, etc.). And the propulsive moment generated from the applied force at the axle has a much shorter moment arm (equal to the wheel radius) than the opposing moment from the net drag force centered near the top of the wheel (with a moment arm substantially exceeding the wheel radius)—since both moment arms are pivoting about the same stationary ground contact point. Thus, for these opposing moments to precisely counterbalance each other, the propulsive force applied at the axle—with the shorter moment arm—must substantially exceed the net drag force near the top of the wheel.

In this way, the horizontal drag forces exerted upon the upper surfaces of the wheel are leveraged against opposing and substantially magnified forces at the axle. Hence, a relatively small frictional drag force centered near the top of the wheel can have a relatively high impact on the propulsive counterforce required at the axle. Shielding these upper wheel surfaces can divert much of these headwind-induced drag forces directly onto the vehicle body, thereby negating much of the retarding force amplification effects due to the pivoting wheel geometry.

Moreover, since the propulsive force applied at the axle exceeds the combined upper wheel drag forces, a lateral reaction force (R, as shown in FIG. 25) upon the wheel is necessarily developed at the ground contact point, countering the combined unbalanced propulsive and drag forces on the wheel: Unless the wheel is accelerating, the reaction force at the ground, together with the upper wheel net drag forces (F+P), combine (A=F+R+P, as shown in FIG. 25) to countervail the lateral propulsive force (A) applied at the axle. This reaction force is transmitted to the wheel through frictional contact with the ground. In this way, an upper wheel drag force is further magnified against the axle. For these multiple reasons, it becomes crucial to shield the upper wheel surfaces from exposure to headwinds.

Given that the propulsive force (A) applied at the axle must overcome both the net wheel drag forces (F+P) and the countervailing lower reaction force (R) transmitted through the ground contact point, it can be shown that the net drag force upon the upper wheel can oppose vehicle motion with nearly twice the sensitivity as an equivalent drag force upon the static frame of the vehicle. Hence, shifting the impact of upper wheel drag forces to the static frame can significantly improve the propulsive efficiency of the vehicle.

Furthermore, as drag forces generally increase in proportion to the square of the effective wind speed, the more highly sensitive upper wheel drag forces increase far more rapidly with increasing headwind speeds than do vehicle frame drag forces. Thus, as the vehicle speed increases, upper wheel drag forces rapidly become an increasing component of the total drag forces retarding vehicle motion.

And given the greater sensitivity of speed-dependent upper wheel drag forces—as compared against vehicle frame drag forces—to the retarding of vehicle motion, considerable effort should first be given to minimizing upper wheel drag forces. And shielding the faster-moving uppermost surfaces of the wheel assembly from oncoming headwinds, by using the smallest effective fairing assembly, is an effective means to minimize upper wheel drag forces.

Contrarily, drag forces on the lower wheel generally oppose vehicle motion with reduced sensitivity compared to equivalent drag forces on the static frame of the vehicle. Propulsive forces applied at the axle are levered against lower wheel drag forces, magnifying their impact against these lower wheel forces. Shielding lower wheel surfaces can generally negate this mechanical advantage, and can actually increase overall drag on the vehicle.

Moreover, as discussed above, headwinds on the static frame generally exceed the speed of winds impinging the lower surfaces of the wheel. Hence, frictional drag forces on the lower wheel surfaces are greatly reduced. Thus, it is generally counterproductive to shield the wheel below the level of the axle. Drag on a vehicle is generally minimized with upper wheel surfaces shielded from headwinds and with lower wheel surfaces exposed to headwinds.

Wheel drag sensitivity to retarding vehicle motion becomes even more significant in the presence of external headwinds. With external headwinds, the effective wind speed impinging the critical upper wheel surfaces can well exceed twice the vehicle speed. Shielding protects the upper wheel surfaces both from external headwinds, and from headwinds due solely to vehicle motion.

Indeed, wheel surfaces covered by the shield are exposed to winds due solely to wheel rotation; headwinds are deflected. The effective drag winds beneath the shield are generally directed tangentially to rotating wheel surfaces, and vary in proportion to radial distance from the axle, reaching a maximum speed at the wheel rim equal to the vehicle speed, regardless of external headwinds. Since drag forces vary generally in proportion to the square of the wind speed, the frictional drag forces are considerably reduced on shielded upper wheel surfaces. Using these wind shields, shielded wheel surfaces are exposed to substantially reduced effective wind speeds and to generally much less than half of the drag forces without shielding.

Diminished drag forces from external headwinds impinging the slower moving lower surfaces of a rolling wheel generally oppose wheel motion with much less retarding torque than drag forces from winds impinging the faster upper surfaces. Indeed, tests demonstrate that with upper shields installed on a suspended bicycle wheel, the wheel will spin naturally in the forward direction when exposed to headwinds. Without the shields installed, the same wheel remains stationary when exposed to headwinds, regardless of the speed of the headwind. And an unshielded spinning wheel will tend to stop spinning when suddenly exposed to a headwind. This simple test offers an explanation for the unexpected result achieved from Greenwell mentioned above—and demonstrates that by minimally shielding only the upper wheel surfaces from external headwinds, the overall drag upon the rotating wheel can be substantially reduced.

Furthermore, as external headwinds upon a forwardly rotating vehicle wheel add relatively little frictional drag to the lower wheel surfaces—which move forward at less than the vehicle speed but add far more significant drag to the upper wheel surfaces, which move forward faster than the vehicle speed and which can more significantly retard vehicle motion, shielding the upper wheel surfaces against headwinds is particularly beneficial. Since drag forces upon the wheel are generally proportional to the square of the effective wind speed thereon, and the additional drag on the wheel—and thereby on the vehicle—increases rapidly with headwinds, shielding these upper surfaces greatly reduces the power required to propel the vehicle. Moreover, the relative effectiveness of shielding upper wheel surfaces generally increases with increasing headwinds.

An examination of the retarding wind vectors on a rotating wheel can reveal the large magnitude of drag retarding moments upon the uppermost wheel surfaces, relative to the lower wheel surfaces. And an estimate of the frictional drag torque on the wheel can be determined by first calculating the average moments due to drag force vectors at various points—all pivoting about the ground contact point—on the wheel (results shown plotted in FIG. 17), and then summing these moments at various wheel elevations above the ground and plotting the results (FIG. 18). The area under the resulting curve (shown in FIG. 18 as a series of curves representing various headwind conditions) then represents the total frictional drag (absent profile drag) torque upon the wheel.

In order to determine the relationship between this torque and elevation on the wheel, the magnitudes of the drag wind vectors that are orthogonal to their corresponding moment arms pivoting about the point of ground contact must first be determined. These orthogonal vector components can be squared and then multiplied by the length of their corresponding moment arms, in order to determine the relative moments due to drag at various points along the wheel rim.

The orthogonal components of these wind vectors tend to increase linearly with elevation for points on the rim of the wheel, and also for points along the vertical mid-line of the wheel. Calculating the moments along the vertical mid-line of the wheel can yield the minimum relative drag moments at each elevation. Calculating an average of the maximum drag moment at the rim combined with the minimum drag moment along the mid-line can then yield the approximate average drag moment exerted at each elevation upon the wheel. Multiplying this average drag moment by the horizontal rim-to-rim chord length can yield an estimate of the drag torque exerted upon the wheel at each elevation level (FIG. 18). These calculations are simply determined from the geometry of the rotating wheel; the object of this analysis is to determine the likely relative magnitudes of drag torques upon the wheel at various elevations.

From the resulting plots (FIG. 18), it can be estimated that the uppermost approximate one-third section of the wheel likely contributes most of the overall drag torque upon the wheel. Thus, by shielding this upper section from headwinds, drag torque can be considerably reduced. With upper-wheel shielding, as noted above, the relative winds beneath the shield are due mostly to wheel rotation, and are generally directed tangentially to the wheel. The resulting drag torque under the shielded sections can then be determined as above, and compared with the unshielded drag torque for similar headwind conditions.

These calculations—generally confirmed by tests—indicate a substantial reduction in retarding drag torque upon the shielded upper wheel surfaces. In the absence of external headwinds, the plots of FIG. 18 indicate that shielding the uppermost approximate one-third section of the wheel can reduce the drag torque of this section considerably, by as much as 75 percent. Moreover, repeating calculations and testing with an external headwind equal to the vehicle speed indicates that upper wheel shielding can reduce the comparative upper wheel drag torque of this section by still more, perhaps by as much as 90 percent. Hence, the potential effectiveness of shielding upper wheel surfaces can be significant, especially with surfaces having higher drag sensitivities, such as wheel spoke surfaces.

As discussed above, since upper wheel drag forces are leveraged against the axle—thereby magnifying the propulsive counterforce required at the axle—an increase in drag force on the wheels generally retards vehicle motion much more rapidly than does an increase in other vehicle drag forces. And while under external headwind conditions, the total drag on a vehicle with wheels exposed directly to headwinds increases still more rapidly with increasing vehicle speed.

Shielding upper wheel surfaces effectively lowers the elevation of the point on the wheel where the effective net drag force is exerted, thereby diminishing the magnifying effect of the propulsive counterforce required at the axle, as discussed above. As a result, the reduction in drag force upon the vehicle achieved by shielding the upper wheel surfaces is comparatively even more significant with increasing external headwinds. Shielding these upper wheel surfaces can thereby improve relative vehicle propulsion efficiency under headwinds by an even greater margin than under null wind conditions.

Moreover, shielding these upper wheel surfaces can be particularly beneficial to spoked wheels, as round spokes can have drag sensitivities many times greater than that of more streamlined surfaces. As round spokes—in some configurations—can have drag coefficients ranging from one to two orders of magnitude greater than corresponding smooth, streamlined surfaces, shielding the spokes of the upper wheel from external wind becomes particularly crucial in reducing overall drag upon the wheel.

Accordingly—given these multiple factors—a relatively small streamlined fairing attached to the vehicle structure and oriented to shield the upper surfaces of the wheel assembly from oncoming headwinds substantially reduces drag upon the wheel, while minimizing total drag upon the vehicle. Consequently, an embodiment includes the addition of such a fairing to any wheeled vehicle—including vehicles having spoked wheels, where the potential drag reduction can be even more significant.

The addition of such minimal fairings to each side of a traditional spoked bicycle wheel, for example, reduces windage losses and improves propulsive efficiency of the bicycle, particularly at higher cycle speeds or in the presence of headwinds, while minimizing cycle instability due to crosswind forces. Since crosswinds are a significant factor restricting the use of larger wheel covers, minimizing the fairing size is also an important design consideration. And minimizing form drag induced by the forward-facing profile of the fairing also will influence the fairing design. The preferred fairing size will likely substantially cover the upper section of the exposed wheel, and be placed closely adjacent to the wheel surfaces, consistent with general use in bicycles. In heavier or powered cycles, design considerations may permit somewhat larger fairings, covering even more of the wheel surfaces.

As shielding upper wheel surfaces can reduce overall drag on the vehicle, while simultaneously augmenting the total frontal profile area of the vehicle exposed to headwinds, a natural design constraint emerges from these competing factors: Shields should be designed sufficiently streamlined and positioned sufficiently close to wheel surfaces to provide reduced overall vehicle drag. And as shielding effectiveness potentially increases under headwind conditions, shields designed with larger surface areas and larger frontal profiles may still provide reduced overall vehicle drag under headwind conditions, if not under null wind conditions. Thus, a range of design criteria may be applied to selecting the best configuration and arrangement of the fairing, and will likely depend on the particular application. In any particular application, however, the embodiment will include a combination of design factors discussed above that will provide a reduction in overall vehicle drag.

In a cycle application, for example, fairings positioned within the width of the fork assembly will likely provide the most streamlined design which both shields spokes from headwinds but also minimizes any additional form drag profile area to the vehicle frame assembly. In other applications, insufficient clearances may preclude positioning the fairings immediately adjacent to moving wheel surfaces. In such situations, headwinds may be sufficient in magnitude to cause a reduction in overall vehicle drag to justify the use of wider upper wheel fairings—positioned largely outside the width of the fork assembly—with extended forward profile areas.

Furthermore, from the previous analysis a consideration the drag torque curves wholly above the level of the axle, it becomes apparent that shielding the wheel is best centered about an elevation likely between 75 and 85 percent of the diameter of the wheel, or near the center of the area under the unshielded torque curve shown in FIG. 18. While drag forces are generally greatest in magnitude near the top of the wheel, the effective exposed topmost surface areas are much smaller, thereby limiting the magnitude of drag torques upon the uppermost surfaces of the wheel. Thus, the upper wheel fairing would best extend above and below this critical level (generally, between 75 and 85 percent of the diameter of the wheel) in order to optimally minimize drag upon the wheel. And as the surfaces forward of the axle are the first to be impacted by headwinds, shielding these surfaces is essential to deflecting headwinds from the rearward surfaces. Thus, the higher-sensitivity drag-inducing surfaces in the forward upper quadrant and centered about this critical elevation on the wheel generally need to be shielded for optimal minimization of drag. These higher-sensitivity drag-inducing surfaces generally centered about this critical elevation and extending to include those surfaces with higher drag-inducing sensitivities that are positioned mostly in the forward upper quadrant of the wheel, but likely also to include much of the wheel surfaces positioned in the rearward upper quadrant, are herein defined and later referred to as: major upper drag-inducing surfaces. And the critical level about which the major drag-inducing surfaces are generally centered in elevation is herein defined and later referred to as: critical elevation.

As discussed, the precise elevation about which the major upper drag-inducing surfaces are centered, as well as the precise extent to which surfaces in the forward quadrant and in the upper half of the wheel central structure are included in the major upper drag-inducing surfaces, will depend on the particular application and operating conditions. Certain wheel surfaces with higher drag sensitivities, such as wheel spokes, generally need to be shielded when positioned within the region of the major upper drag-inducing surfaces. Other surfaces such as smooth tire surfaces having lower drag sensitivities may also benefit from shielding if their surface areas are extensive, are positioned near the critical level in elevation, or are the primary upper wheel surfaces exposed to headwinds. In the example analysis of FIGS. 17 and 18, a uniform surface across the wheel having a constant drag-sensitivity was assumed. In any particular application, the unique combination of different wheel surfaces with differing drag sensitivities will determine the particular height of the critical elevation level about which the major upper drag-inducing surfaces are centered.

A similar analysis can be performed for form drag forces on the moving forward vertical profiles of the wheel rim or tire. The results obtained are generally similar in form, though may differ somewhat in magnitudes as the effective wind speeds on the moving profiles are generally lower on the upper wheel—equal to the vehicle speed—and will depend on the particular application, including the total area of the wheel forward profile exposed to headwinds, and to headwind and vehicle speeds. Nevertheless, the net pressure drag torque caused by the moving outline of the wheel is also centered above the level of the axle, and thereby merits consideration in determining the particular height of the critical elevation level, and in the ultimate configuration of the fairing.

Hence, the fairing shown in FIG. 1 is best configured to shield the uppermost and forward wheel surfaces, and to extend rearward to at least partially shield the forward profile of the trailing portion of the upper wheel rim, consistent with the further requirement to extend downward as much as practical to the level of the axle. Furthermore, the fairing surface area is best limited in total extent, and the forward facing fairing profile is best limited in both lateral and vertical projection apart from the wheel, to cause a substantial reduction in total vehicle drag. And as mentioned, crosswind considerations will also influence the ultimate configuration for a particular application.

From these considerations it also becomes apparent that a new method of minimizing drag on a vehicle has been identified. Vehicle drag can be minimized by shielding the headwind from otherwise impinging the primary vehicle-drag inducing wheel surfaces, which have stronger effective headwinds otherwise impinging thereon. Shielding these upper wheel surfaces can yield substantial reductions in overall vehicle drag through reducing the net drag-induced resistive force, which would otherwise be applied higher on said wheel assembly near the level of the critical elevation than the countervailing vehicle propulsive counterforce which is applied lower in elevation at the axle.

Moreover, as the net drag-induced resistive force also has a substantial mechanical advantage over the countervailing vehicle propulsive counterforce, since both the resistive force and the counterforce are levered in opposition about the same lowermost stationary point of ground contact on said wheel assembly, vehicle drag reduction by shielding the upper wheel surfaces is enhanced even further. A drag force on the fairing—which is attached to the vehicle frame is countervailed through the vehicle frame from a propulsively driven wheeled axle of the vehicle. The propulsive axle provides a proportional propulsive countertorque equivalent to a countervailing propulsive force being transmitted from the wheel assembly and applied to the vehicle frame at the level of the axle. Thus, the drag on the fairing has no mechanical advantage over the countervailing propulsive force, since both the fairing drag force and the countervailing propulsive force are in direct opposition at the same level at the axle. Thus, shielding provided by the fairing shifts drag otherwise induced on the mechanically-advantaged critical upper wheel surfaces to the slower-moving mechanically-equivalent vehicle frame surfaces.

Finally, for similar reasons as above, reducing the drag on the upper wheel surfaces by means other than shielding can also reduce drag on the vehicle, as will be shown in other embodiments. In consideration of further embodiments described below, the operating principles described above will generally apply, and may be referred thereto.

Second Embodiment Description FIG. 2

As shown in FIG. 2, a streamlined fender 7 is attached to the inside of the front-fork tube assembly 2 of a typical cycle having spoked wheels 4 with studded tires 8. The fender 7 is positioned closely adjacent to tire 8, covering the approximate upper and front-most quadrant of the tire 8, and is rigidly fixed to the stationary portion of axle assembly 9 using struts 10. The fender 7 has sufficient structural rigidity to allow close placement to tire 8, thereby minimizing any oncoming headwinds from leaking between tire 8 and fender 7.

With fender 7 configured in this way, the treads near the top of the tire 8 are shielded from headwinds. Shielded this way, the topmost surfaces of tire 8 are moving at an effective wind speed closer to the ground speed of the cycle, rather than moving with respect to the oncoming external wind at an effective speed of up to nearly twice the ground speed of the cycle. As a result, the aerodynamic drag forces exerted upon the upper treads of tire 8 are substantially reduced.

The reduction drag force has the greatest effect near the top of tire 8, where the surfaces of tire 8 are moving fastest with respect to external winds otherwise impinging thereupon. As the uppermost surfaces of tire 8 rotate away from the topmost point to an intermediate position with respect to either of two lateral midpoints on the tire 8, these drag forces are greatly reduced. Thus, the embodiment shown in FIG. 2 covers this critical uppermost and forward-oriented quadrant of tire 8, minimizing the addition of unnecessary weight and drag-inducing structure to the cycle.

Second Embodiment Operation FIG. 2

An embodiment including a forwardly oriented fender 7, shielding the uppermost outer surfaces of the tire 8 from oncoming headwinds, can offer not only similar aerodynamic benefits to fairing 1 of FIG. 1 in reducing frictional drag forces on tire surfaces, but can also substantially reduce form drag forces on the wheel's forwardly facing profiles.

As discussed above, both frictional and pressure drag forces can be shown to exert moments of force pivoting about the point of ground contact. And these forces are magnified against the propulsive force required at the axle. And as such, either type of drag force exerted upon the upper wheel retards vehicle motion considerably more than a similar force exerted either upon a lower surface of the wheel, or directly upon the frame or body of the vehicle. Minimizing these upper wheel drag forces is therefore critical to improving propulsive efficiency of the vehicle.

Fender 7 is an effective means to minimize both frictional drag forces on upper wheel surfaces, and pressure drag forces exerted on the upper wheel. Fender 7 shields tire 8 from headwinds and thereby reduces drag on surfaces of tire 8. Fender 7 also deflects headwinds from tire 8 and thereby shifts headwind form drag forces normally directed upon the upper wheel forward profile to be instead directed upon the vehicle frame. Thus, fender 7 reduces wheel form drag force (as well as tire frictional drag force) magnification effects significantly.

And similar to the first embodiment of FIG. 1, the optimum design for a particular headwind application will size fender 7 sufficiently extensive in frontal profile area to effectively shield tire 8 from headwinds, but sufficiently narrow to minimize any added form drag to the vehicle, and which will result in an overall reduction in vehicle drag. For certain wheels having tires with rough, high-drag sensitivity tread patterns, such a topmost and forwardly-oriented fender 7 can provide sufficient reduction in total upper tire drag to offset any added vehicle drag from the fender itself. In higher speed vehicles, particularly those having wider tires exposed directly to headwinds—such as certain jeep-type automobiles or trucks—using an upper and forwardly-oriented fender 7 to shield the upper wheel surfaces may offer dramatic reductions in vehicle drag.

Third Embodiment FIG. 3

Similarly, as shown in FIG. 3, a streamlined combination fender and fairing assembly 12 is attached to the inside of front fork tube assembly 2 of a typical cycle having spoked wheels 4. The fender portion of the combination assembly 12 is positioned closely adjacent to the tire 8 covering the approximate upper and front-most quadrant of the tire 8. The fairing portions of the combination assembly 12 are positioned closely adjacent to the inner wheel structure of wheel 4 covering the approximate upper and front-most quadrant on each side of wheel 4. The combination assembly 12 is provided sufficient structural rigidity to allow close placement to wheel 4 and tire 8, thereby minimizing any oncoming headwinds from leaking either between tire 8 and the fender portion of the combination assembly 12, or between the inner structure of wheel 4 and the fairing portions of the combination assembly 12.

With the combination fender and fairing assembly 12 configured in this way, both the spokes 5 and the treads of tire 8 near the top of the wheel 4 are shielded from headwinds. And similar to the embodiments of FIG. 1 and FIG. 2, the aerodynamic drag forces exerted upon the topmost spokes 5 and the upper treads of tire 8 are substantially reduced, and thereby may offer dramatic reductions in vehicle drag.

In addition, however, including fairing assembly 12 in this embodiment provides an additional measure of profile shielding to the frontal area of the trailing upper section of wheel 4, thereby further reducing total wheel profile form drag. And similar to the second embodiment of FIG. 2, the optimum design for a particular headwind application will size combination fender and fairing assembly 12 sufficiently extensive in both frontal profile area and fairing size to effectively shield surfaces of wheel 4 and tire 8 from headwinds, but sufficiently narrow and compact in size to minimize any added drag to the vehicle, and which will result in an overall reduction in vehicle drag.

Fourth Embodiment FIG. 4

As shown in FIG. 4, a streamlined fender 7 is attached to a typical sports car 13 having otherwise exposed tires 8. The fender 7 is positioned closely adjacent to the tire 8, covering the approximate upper and front-most quadrant of tire 8. The fender 7 is attached either to the moving wheel suspension assembly of wheel 4, thereby minimizing any relative motion between the suspended wheel 4 and the fender 7, or directly to the body structure of car 13 with the wheel suspension displacement range substantially constrained. The fender 7 is provided sufficient structural rigidity to allow close placement to tire 8, thereby minimizing any oncoming headwinds from leaking between tire 8 and fender 7.

With fender 7 configured in this way, the tread near the top of tire 8 is shielded from headwinds. And similar to the embodiment of FIG. 2, the aerodynamic drag forces exerted upon the upper surfaces of tire 8 are substantially reduced, and thereby may offer dramatic reductions in vehicle drag.

Fifth Embodiment FIG. 5

As shown in FIG. 5, a streamlined combination fender and fairing assembly 12 is attached to a typical sports car 13 having otherwise exposed tires 8 and spoked wheels 4. The fender portion of the combination assembly 12 is positioned closely adjacent to the tire 8 covering the approximate upper and front-most quadrant of the tire 8. The combination assembly 12 is attached either to the moving wheel suspension assembly of wheel 4, thereby minimizing any relative motion between suspended wheel 4 and combination assembly 12, or directly to the body structure of car 13 with the wheel suspension displacement range substantially constrained. The fairing portions of combination assembly 12 are positioned closely adjacent to the inner wheel structure of wheel 4 covering the approximate upper and front-most quadrant on each side of wheel 4. The combination assembly 12 is provided structural rigidity sufficient to allow close placement to wheel 4 and tire 8, thereby minimizing any oncoming headwinds from leaking either between tire 8 and the fender portion of combination assembly 12, or between the inner structure of wheel 4 and the fairing portions of combination assembly 12.

With the combination fender and fairing assembly 12 configured in this way, both the spokes 5 and the treads of tire 8 near the top of the wheel 4 are shielded from headwinds. And similar to the embodiment of FIG. 3, the aerodynamic drag forces exerted upon the upper spokes 5 and the upper surfaces of tire 8 are substantially reduced, and thereby may offer dramatic reductions in vehicle drag.

Sixth Embodiment Description FIG. 6

As shown in FIG. 6, a streamlined wind-deflecting fairing 14 is shown attached to a typical sports car 13 having otherwise exposed tires 8. The wind-deflecting fairing 14 is positioned slightly forward and closely adjacent to the tire 8, shielding the approximate upper front-most quadrant of tire 8 from headwinds. The wind-deflecting fairing 14 is attached either to the moving wheel suspension assembly of wheel 4, thereby minimizing any relative motion between the suspended wheel 4—and tire 8—and wing fairing 14, or directly to the body structure of car 13 with the wheel suspension displacement range substantially constrained. The wind-deflecting fairing 14 is designed with minimal surface area, but with sufficient area to deflect headwind from otherwise impinging upon the upper surfaces of tire 8.

With wind-deflecting fairing 14 configured in this way, the tread near the top of tire 8 is shielded from headwinds. And similar to the embodiments of FIGS. 2, 3, 4 and 5, the aerodynamic drag forces exerted upon the upper surfaces of tire 8 are substantially reduced, and thereby may offer dramatic reductions in vehicle drag.

Sixth Embodiment Operation FIGS. 6 and 25

As indicated above, a countervailing ground reaction-force (R, as shown in FIG. 25) opposing vehicle forward motion is naturally developed upon the wheel, primarily in response to the upper-wheel drag forces. This reaction force is transmitted to the wheel through frictional ground contact with the tire. As the net drag force grows generally with the square of the average effective wind speed upon the wheel, these frictional ground contact forces increase in similar proportion.

As a result, proportional down-forces must somehow be developed upon the wheel in order to maintain firm contact with the ground, preventing tire skidding and loss of vehicle control. These down-forces are generally developed using drag-inducing wings and body moldings on the vehicle, often greatly reducing the propulsive efficiency of the vehicle.

Introducing wind-shielding fairings to the upper wheel areas can reduce both the drag forces acting thereon, and the drag inducing down-forces needed to maintain firm ground contact. And the use of a minimal wind-deflecting fairing that also provides a measure of down-force can be particularly beneficial in high-speed vehicle applications. Thus, the use of minimal wind-deflecting upper wheel fairings can further improve both the propulsive efficiency and directional stability of many higher-speed vehicles.

Seventh Embodiment Description FIG. 7

In FIG. 7, a streamlined fairing 1 is shown as in FIG. 1, but includes an adjustable fairing section 15 pivoting at attachment point 16, whereby the total effective area of the combined fairing assembly—shielding the wind from wheel surfaces—can be adjusted to accommodate different crosswind conditions.

Seventh Embodiment Operation FIG. 7

A further embodiment may include adjustable means for varying the exposed surface area of the fairing 1, thereby providing adjustment to the effective shielding of the wheel 4 from oncoming headwinds. Such a fairing mounted on a bicycle, for example, could be collapsed under high crosswind conditions for minimal exposed area, covering only the very topmost surfaces of the wheel, and thereby minimizing potential crosswind forces directed upon the wheel. Under normal wind conditions, the fairing could be extended, covering more of the critical upper-wheel surfaces, thereby maximizing propulsive efficiency.

Adjustable fairing means could also include streamlined holes or slots in the fairing, arranged for minimal drag, but otherwise enabling some crosswinds to penetrate the fairing. While some loss in potential reduction in drag may result from utilizing such perforated means in the fairing, under higher crosswind conditions this configuration may become desirable.

Finally, and particularly for higher speed applications, automatic means for adjustment of the fairing area could be provided to automatically optimize the exposed fairing area for changing operating conditions.

Eighth Embodiment Description FIGS. 8, 9, 10, 11, 12 and

In FIGS. 8 and 9, several examples of prior-art wheels typically found on high-performance automobiles are shown, having outwardly oriented square-profile spokes, which are generally exposed to headwinds. The square cross-sectional profile of prior art spokes is shown in FIG. 10. The streamlined cross-sectional oval profile of the embodiment spokes is shown in FIG. 11. FIG. 12 shows an example of a wheel with generally oval cross-sectional spokes. FIG. 13 shows an example of a wheel with generally oval cross-sectional spokes where the spokes are shown in two rows, one row being offset more toward the inside of the wheel, thereby increasing the strength of the wheel in the axial direction.

Eighth Embodiment Operation FIGS. 8, 9, 10, 11, 12, 13 and

Square spokes have higher sensitivity to drag than either round or more streamlined oval-shaped spokes. Given the importance—established above—of reducing the drag on rotating wheel surfaces over that on other vehicle surfaces, it becomes evident that considerable effort should be given to reducing spoke drag on high-speed wheels.

Thus, an embodiment includes the use of tapered, generally oval-shaped spokes on automotive wheels, especially on wheels with spokes directly exposed to headwinds. For example, the use of an oval-profiled spoke with a two-to-one dimensional ratio may reduce drag by a factor of two or more, over a similar square-profile spoke. And further streamlining the spoke can reduce drag sensitivity even more.

As axial forces upon the wheel are transmitted more efficiently with spokes having square profiles than with streamlined spokes, streamlined designs for automotive spokes may have been largely overlooked. Streamlined oval profiled spokes can provide sufficient axial strength by offsetting the streamlined spokes in the axial direction within the wheel as shown in FIG. 13, and by providing a nonparallel arrangement between the offset rows of spokes as shown in FIG. 33. Using a relatively thin streamlined spoke, in nonparallel arrangement with other similar spokes offset axially (and likely circumferentially) within the wheel, adequate axial structural rigidity can be obtained.

And similar to other embodiments, the aerodynamic drag forces exerted upon the spokes, when positioned in the critical upper wheel region, are substantially reduced. The reduced drag sensitivity of the streamlined spoke used in high-speed automotive wheels can significantly improve vehicle performance—reducing fuel consumption—and traction, especially at higher vehicle speeds and under headwind conditions.

Ninth Embodiment Description FIGS. 14, 15 and 16

In FIG. 14, a streamlined spoke tailfin 20 is installed over a round wire spoke 21—shown in cross-section A-A of FIG. 15—typically used on a cycle. Pivoting rings 22 affixed to tailfin 20 enable tailfin 20 to swivel about the spoke 21, and thereby permitting tailfin 20 to automatically adjust its orientation in response to varying crosswinds. In FIG. 15, the wider profile of the spoke tailfin 20 is shown rotatably attached to spoke 21. In FIG. 16, several spoke tailfin covers 23 of different sizes—shown in the configuration of a cover but similar in streamlined profile to tailfin 20 shown in FIG. 14—are shown installed on a spoke 21. The tailfin cover 23 includes a through-hole containing spoke 21 within its length, enabling the tailfin cover 23 to swivel about spoke 21, and thereby permitting tailfin cover 23 to automatically adjust its orientation in response to varying crosswinds.

Ninth Embodiment Operation FIGS. 14, 15 and 16

The streamlined profile of the swiveling spoke tailfin may offer greatly reduced drag over round spokes, without the potential increase in drag sensitivity of bladed spokes exposed to crosswinds. Use of the streamlined spoke tailfin may reduce drag sensitivity of the round spoke considerably, in some instances by up to a factor of 10.

Eliminating crosswind turbulence upon the streamlined profile is essential to minimize drag on the spokes under crosswind conditions. The relative crosswind-to-headwind vector directed on a point on the wheel varies significantly with wheel rotation. Near the top of the wheel, headwinds are strongest, and any relative crosswinds are less significant. Near the bottom of the wheel, headwinds are minimized and crosswinds are thereby more significant relative sources of drag on the wheel surfaces. Allowing the spoke tailfin to swivel enables the tailfin to adjust to immediate relative crosswinds, which can vary continually with the rotation of the wheel.

The spoke tailfin can be designed either to extend the entire length of the spoke, or to extend over only a portion of the spoke, such as over the outermost section of the spoke nearest the rim, which moves fastest near the top of the wheel, and is thereby exposed to the fastest headwinds.

Alternatively, the spoke tails may be divided in several independent sections along the length of the spoke, allowing independent adjustment to the varying crosswind components along the radial direction of the wheel. And these tailfin sections can be different in both size and configuration, to best minimize drag, as shown in FIGS. 16 and 41. For example, tailfin sections nearest the rim—at the top in FIGS. 16 and 41—are exposed to the faster headwinds and may be designed for more extensive streamlining, while sections closer to the hub—at the bottom in FIGS. 16 and 41—being exposed to slower headwinds and greater relative crosswind vector components, may be designed more compactly for more rapid re-orientation. Or the tailfin could be configured with a tapered cross-sectional profile similar in form to the tapered spoke embodiment, described below and referenced in FIGS. 19-23 and in FIGS. 34-38 which varies along its entire length. This tailfin design could also be used on a vehicle radio antenna, reducing drag and thereby improving fuel consumption for vehicles, especially when operating at highway speeds.

While shielding the spokes with a fairing is an effective means of reducing drag due to headwinds, drag induced solely from winds due to wheel rotation remains largely unaffected. Indeed, the spokes on the lower half of the wheel are relatively less affected by headwinds, and are more affected by the vector components of wind due to wheel rotation. Using streamlined spoke tailfins, drag on the lower spokes can also be reduced. Moreover, swiveling spoke tailfin covers used in conjunction with upper wheel fairings can offer significant reduction in overall drag upon the wheel—and thereby on the vehicle—while minimizing sensitivity to crosswinds.

And similar to other embodiments, the aerodynamic drag forces exerted upon the spokes having attached tailfins, when positioned in the critical upper wheel region, are substantially reduced. Thus, this embodiment may offer dramatic reductions in vehicle drag, particularly when crosswinds are also present.

Tenth Embodiment Description FIGS. 19-23 and 34-39

In FIGS. 19 and 20, and in FIGS. 34 and 35, a streamlined spoke for use in racing-style bicycle wheels, tapers in the broader width from the wheel rim toward the wheel hub. In FIGS. 21 and 36, the profile—shown in cross-section—of the more streamlined end of the spoke is shown. The spoke profile varies along the length of the spoke—from rim toward the hub—with the more thin and streamlined part nearest the rim and the more circular part toward the hub. In FIGS. 22 and 37, the substantially oval profile—shown in cross-section—of the middle of the tapered section of the spoke is shown. In FIGS. 23 and 38, the more rounded profile—shown in cross-section—of the spoke near the end of the tapered section is shown.

The profile is shaped to maintain a generally constant total area in cross-section, in order to retain a relatively constant tensile strength along the full length of the spoke. The spoke profile may include cross-sectional areas varying somewhat along the spoke length, typically with larger areas nearest the ends of the spoke to enhance strength near attachment points. Nearest the wheel rim, the streamlined profile is more elliptical (or flat like a blade or thin wing), as shown in FIGS. 21 and 36, while toward the hub the profile becomes more closely circular—as shown in FIGS. 23 and 39. While the general trend for tapering the spoke is as shown, the particular application will determine just how thin and wide the spoke is near the rim, and how rapidly the tapered section becomes more oval or circular in cross-sectional profile toward the hub.

Tenth Embodiment Operation FIGS. 19-23 and 34-39

Streamlined spokes reduce drag upon the wheel in the presence of direct headwinds. A crosswind directed upon the wheel can cause turbulence across the broad face of the streamlined spoke, quickly increasing drag thereon. Eliminating crosswind turbulence upon the streamlined profile is essential to minimizing drag under crosswind conditions. The design challenge becomes to minimize drag through spoke streamlining over the widest range of crosswind conditions; too wide a blade design can exacerbate drag under even minimal crosswinds, thereby negating any advantage of the streamlined spoke profile.

Notably, the relative crosswind-to-headwind vector component varies significantly depending on the relative location on the wheel. Near the top of the wheel, headwinds are strongest, and any relative crosswinds are less significant. Near the bottom of the wheel, headwinds are minimized and crosswinds are more significant. Thus, crosswinds can be a more significant relative source of drag on wheel surfaces closer to the ground.

The broader width of the bladed spoke provides greater streamlining for the higher speed headwinds near the top of the wheel, thereby minimizing drag on these critical drag-inducing surfaces. Any turbulence from the relatively smaller crosswind components directed upon the faster moving uppermost portion of the bladed spokes is generally minimized. The same crosswinds directed upon slower moving spoke surfaces near the center of the wheel are a more significant relative component of the total wind vector thereon, and thus have a greater potential to induce turbulence—and thereby to increase drag.

And as lower surfaces of the wheel are exposed to substantially reduced headwinds, and also contribute much less resistive torque upon the wheel, crosswind-induced turbulence on the lower spokes is a relatively insignificant factor contributing to overall vehicle drag when compared to the upper wheel surfaces. Thus, spoke profiles are best tapered for optimum reduced drag on upper wheel surfaces, rather than for lower wheel surfaces.

As a circular spoke profile generally produces far less drag-inducing turbulence than a flat blade profile when obliquely facing the wind, the portion of the spoke most sensitive to crosswinds should be closer to circular in profile, while the portion of the spoke less sensitive to crosswinds should be closer to a streamlined wing shape in profile. Thus, a tapered spoke—whose profile gradually transitions from thin and streamlined near the rim of the wheel, to more oval or circular toward the central hub of the wheel—can reduce the drag on the spoke over a wider range of crosswind conditions than traditional generally constant cross-sectional profile—either bladed or circular—spoke designs. The degree of tapering needed from the rim toward the hub will vary depending on the relative crosswind component for any particular application; applications with greater crosswind components would benefit more from more rapid tapering, where the spoke become rounded in cross-section near the middle of the spoke, rather than nearer to the hub.

Furthermore, the tapered spoke may be designed to transition in cross-sectional profile in a step-wise manner—from a streamlined bladed profile near the rim to a more rounded cross-sectional profile toward the hub. Such a tapered spoke design with a sufficient number of step-wise transitions separating substantially constant profile longitudinal sub-sections of the spoke, may offer similar performance to the smoothly-varying transition design with reduced fabrication costs.

And similar to other embodiments, the aerodynamic drag forces exerted upon the spokes, when positioned in the critical upper wheel region, are substantially reduced. Thus, this embodiment may offer dramatic reductions in vehicle drag, particularly when crosswinds are also present.

Eleventh Embodiment FIGS. 26, 27, 28, 29 and 30

In FIG. 27, an aggressive tire tread block pattern is shown having tread blocks which taper smoothly in profile on the leeward side, thereby reducing drag. The tread blocks are spaced apart and arranged to permit air displaced by the tread to flow smoothly between, around and over each block, minimizing any flow separation—and thereby turbulence—behind each individual tread block. The relatively sharp, angular windward side of each block thereby provides for aggressive traction for typical off-road vehicle applications. However, the smoother leeward side of each tread block provides substantial streamlining for upper wheel drag reduction.

Tires using these streamlined tread blocks are thereby typically designed for unidirectional rotation, since using these tires in reverse rotation may reduce traction. Forward-facing windward surfaces of the tread blocks are generally sharp and angular in shape, and are thus optimized for maximum traction on slippery ground; while the leeward, rearward-facing surfaces of the tread blocks are streamlined in design in order to reduce drag on each block.

The tread blocks are spaced and arranged to provide sufficient clearances to allow generally minimally restricted air flow there-between, such that air flowing near the top of the tire is deflected substantially between the tread blocks, rather than mostly over the top of the tire. Near the top of the wheel assembly within the forward quadrant, air flowing around one block is largely diverted between the blocks, with minimal diversion of air over the top surface of the block. And tread blocks are generally arranged to direct diverted air largely toward the leeward side of adjacent blocks. In this way, the pressure differential between the windward and leeward surfaces of tread blocks is further minimized, thereby reducing form drag on the tread blocks even more.

With tire tread blocks configured in this way, the tread near the top of tire is substantially streamlined for impinging headwinds. Form drag upon the tread blocks is thereby substantially reduced, both where winds most directly impinge the windward tread block surfaces, and where the fastest moving tread blocks are located—near the top of tire. As discussed above, these uppermost wheel surfaces are also the most critical drag-inducing surfaces retarding vehicle motion and increasing down-forces needed to maintain tire traction at higher speeds. Thus, it becomes crucial to minimize drag on these upper tire tread blocks. And streamlining tread patterns for this location on the wheel assembly is an effective means to improve propulsive efficiency of the vehicle, particularly at higher vehicle speeds.

Various configurations of tread patterns may incorporate streamlined tread blocks for reducing upper wheel drag forces against the tire. Tread blocks may taper either in width, depth or length. Alternative tread block patterns may incorporate more or less streamlined tapered lengths, depending on the application; longer streamlined blocks may reduce the total number of tread blocks available to cover the tire, enhancing drag reduction for higher speed applications at the expense of somewhat reduced tire traction. Contrarily, shorter streamlined blocks may increase the total number of tread blocks available to cover the tire, enhancing tire traction for slower speed applications at the expense of somewhat reduced drag reduction.

Windward tread block surfaces may also include somewhat oblique patterned arrangements—as shown in FIG. 28—rather than a more parallel orientation to the wheel axle often used to maximize traction. Alternatively, both windward and leeward tread block surfaces may include streamlined designs, with the blocks being more substantially oval in shape; the oval blocks can be shaped either symmetrically-similar from front to back such as in FIGS. 29 and 30, or the windward side can be shaped to be more sharp and angular, with the leeward surface being more streamlined and extended in length. In either case, sufficient clearance between the tread blocks must be maintained in order to enable substantial air flow there-between, and to enable pressure relief behind adjacent tread blocks, thereby minimizing form drag on the blocks. And for each of these embodiments, tread blocks are arranged in an aerodynamically optimized pattern.

In order to maintain adequate pressure on trailing block surfaces, the lateral clearance space between laterally-spaced adjacent blocks should be restricted in order to divert sufficient air flow to cause substantially increased pressure on trailing block surfaces. In most embodiments, this clearance should be restricted to no more than half the lateral width of the tread blocks. Too narrow a clearance between the blocks will not allow sufficient air flow to cause increased pressure on the trailing surfaces in order to reduce form drag on the blocks. Thus, a natural design constraint emerges from these two competing factors between too wide and too narrow lateral clearances between the blocks, which will vary depending on the nominal operating condition for each particular application.

Finally, while the pattern of thread blocks shown demonstrates an optimum aerodynamic configuration, addition non-aerodynamic tread blocks may be introduced within the aerodynamic pattern in order to achieve other purposes. For example, a few properly designed tread blocks may be spaced to interrupt the aerodynamic pattern in order either to reduce noise or to increase traction for reverse rotation of the wheel. However, in order to ensure the primary purpose of reduced drag on the tire, a majority of the tread blocks will likely remain optimized for streamlined aerodynamic purposes.

And similar to other embodiments, the aerodynamic drag forces exerted upon the upper surfaces of tire are substantially reduced. Thus, this embodiment may offer dramatic reductions in vehicle drag, particularly for faster vehicles with aggressively treaded tires that are exposed directly to headwinds.

Twelfth Embodiment Description FIGS. 31 and 32

As shown in FIG. 32, a wind-deflecting exhaust pipe array 34 is shown on one side of a typical top-fuel dragster race car 30, where the exhaust pipes are directed laterally in a distributed fashion to divert headwinds from directly impinging the upper surfaces of the rearmost exposed tire 36. The extreme velocity of the air emanating from the exhaust pipes is used to deflect the headwinds generally above the uppermost surfaces of the rear tire. Rather than aligning the pipes all in an aligned array 32 with pipes directed mostly upward but substantially toward the outside of the vehicle—as is commonly seen in the racing art as shown in FIG. 31—the pipes in this embodiment are arranged to direct the exhaust upward, but spanning the entire width of the rear tire. Properly positioned for the particular application, the ejected exhaust gases deflect substantial headwinds upward above the rear tire 36.

With the wind-deflecting exhaust pipe array 34 configured in this way, the surfaces near the top of rear tire 36 are substantially shielded from impinging headwinds. And similar to the embodiment of FIG. 6, the aerodynamic drag forces exerted upon the upper surfaces of rear tire 36 are substantially reduced, and may thereby offer dramatic reductions in high speed vehicle drag forces.

Variations on this embodiment are easily envisioned, and could be employed wide variety of more traditional sports cars, automobiles, and motorcycles. For example, exhaust pipes could be directed to exit in the upper forward portion of the fender well, directing exhaust gases sideways out the front of the well, thereby helping to shield the upper wheel surfaces from headwinds.

Advantages

From the description above, a number of advantages of some embodiments become evident:

-   (a) The addition of simple upper wheel fairings to a bicycle can     improve rider propulsive efficiency—especially in headwinds—without     compromising rider comfort, significantly increasing wheel expense     or decreasing wheel durability. -   (b) The addition of simple upper wheel fairings to an electric     bicycle powered by rechargeable batteries can improve motor     propulsive efficiency, especially in headwinds, extending the     effective range of such power-assisted bicycles. -   (c) The addition of simple upper wheel fairings to a motorcycle can     improve propulsive efficiency—especially in headwinds—yielding     greater fuel economy. -   (d) The addition of simple upper wheel fairings to certain     automobiles having otherwise exposed tires, such as jeep-type     vehicles with elevated suspensions, can improve propulsive     efficiency—especially in headwinds—yielding greater fuel economy. -   (e) The addition of simple upper wheel fairings to certain truck and     trailer wheels having otherwise exposed tires can improve propulsive     efficiency—especially in headwinds yielding greater fuel economy. -   (f) The addition of simple upper wheel fairings to a bicycle or     motorcycle can reduce the down-force needed to ensure cycle     stability—especially important when navigating curved roads under     wet conditions—thus also better sustaining cornering traction during     intermittent wind gusts, and thereby improving cyclist safety. -   (g) The addition of simple upper wheel fairings to certain     high-speed vehicles having otherwise exposed tires can reduce the     down-force needed to ensure vehicle stability. Reducing down-force     in turn reduces the need for drag-inducing wings. In addition,     reducing down-force results in reduced tire rolling resistance and     bearing friction. These factors thereby improve propulsive     efficiency—especially in headwinds—yielding greater fuel economy. -   (h) The use of streamlined spokes in automotive wheels—especially in     wheels used in certain high-speed vehicles having otherwise exposed     spokes—can reduce both drag on the upper wheel and consequently the     down-force needed to ensure vehicle stability, and thereby improve     propulsive efficiency and vehicle safety—especially in     headwinds—yielding greater fuel economy. -   (i) The use of axially offset streamlined spokes in automotive     wheels—especially in wheels used in certain high-speed vehicles     having otherwise exposed spokes—can reduce both drag on the upper     wheel and consequently the down-force needed to ensure vehicle     stability, while maintaining the axial strength of the wheel. This     in turn can improve propulsive efficiency and vehicle     safety—especially in headwinds—yielding greater fuel economy. -   (j) The use of streamlined spoke tailfins in cycle wheels—especially     in wheels having otherwise exposed spokes—can reduce both drag on     the upper wheel and consequently and the down-force needed to ensure     vehicle stability, and thereby improve propulsive efficiency and     cycle safety, especially in headwinds. -   (k) The use of variably-tapered spokes in cycle wheels, where the     spokes are tapered from a streamlined profile near the rim to more     oval or circular profile toward the wheel hub can reduce both drag     on the upper wheel and consequently the down-force needed to ensure     cycle stability, and thereby improve propulsive efficiency and cycle     safety—especially in headwinds—over a wide range of crosswind     conditions. -   (l) The use of tires having streamlined tread blocks arranged in an     optimal aerodynamic pattern can reduce both drag on the upper wheel     and consequently the down-force needed to ensure vehicle stability,     and thereby improve propulsive efficiency and vehicle     safety—especially in headwinds—yielding greater fuel economy. -   (m) The use of vehicle engine exhaust pipes arranged in an optimal     pattern to direct exhaust gases to deflect headwinds from otherwise     impinging upper wheel surfaces can reduce both drag on the upper     wheel and consequently the down-force needed to ensure vehicle     stability, and thereby improve propulsive efficiency and vehicle     safety—especially in headwinds—yielding greater fuel economy.

CONCLUSIONS, RAMIFICATIONS, AND SCOPE

Exposed wheels can generate considerable drag forces on a moving vehicle. These forces are directed principally near the top of the wheel, rather than being more evenly distributed across the entire profile of the wheel. Moreover, these upper-wheel drag forces are levered against the axle, thereby magnifying the counterforce required to propel the vehicle. As a result, a reduction in drag upon the upper wheel generally enhances propulsive efficiency significantly more than a corresponding drag reduction on other parts of the vehicle.

With the net drag forces being offset and directed near the top of the wheel, nearly equivalent countervailing reaction forces—also opposing vehicle motion—are necessarily transmitted to the wheel at the ground. These reaction forces necessitate augmented down-forces to be applied in higher speed vehicles, in order to maintain static frictional ground contact and, thereby, vehicle traction and directional stability. As wings and other means typically used to augment these down-forces in such vehicles can add significant drag, it becomes evident that substantial effort should be made to reduce the upper wheel drag forces on most high-speed vehicles.

Modern automobile wheels, particularly those designed for use with low-profile tires typically found on expensive sports cars, often include narrow spoke sections connecting the hub and rim, which become significant sources of drag. Recent automotive design innovation on sports cars has focused on reducing upper-body drag while simultaneously increasing down-forces to maintain traction. However, the wheel spokes typically used remain configured with inefficient drag profiles, and are often located on the outside of the wheel assembly, where they can be more directly exposed to headwinds. These spokes often have generally rectangular cross-sectional profiles, which present significantly increased sensitivity to drag forces upon the upper wheel, and thereby upon the vehicle.

An embodiment includes the use of aerodynamic profiles on the spokes of automotive wheels, designed to minimize drag. By shaping the spokes in an oval cross-sectional profile with a two-to-one dimensional ratio, for example, the drag sensitivity can generally be reduced by a factor of two or three times over a corresponding square-profile spoke design. Further narrowing of the streamlined profile can reduce drag sensitivity of the spokes even more. Given the magnifying property of upper wheel drag forces to increasing both the down-forces needed to maintain vehicle traction and the overall drag upon the vehicle, configuring exposed spokes for minimal drag can be particularly helpful to improving vehicle propulsive efficiency, especially for the outermost spokes and for wheel sections nearest the rim which are most exposed to headwinds.

Drag can be reduced on the narrow round spokes of bicycle wheels, by simply adding a streamlined tailfin section to the leeward side of the spoke. By enabling the streamlined tailfin to swivel about the spoke in response to varying crosswinds, drag can be minimized over a variety of crosswind conditions over the full range of wheel rotation. And several tailfins of varying configurations can be used in combination to optimize drag on the spoke, in response to variable crosswinds along the length of the spoke on the upper wheel.

Alternatively, drag can be reduced on the bladed spokes of bicycle wheels, by simply by tapering the blade of the spoke at the rim to a more round profile toward the wheel hub. By tailoring the profile of the spoke to accommodate the range of crosswind components—which vary in magnitude from the rim to the hub—drag can be minimized on the spoke over a variety of crosswind conditions. Moreover, the tailfin could also be adapted with a similar variable cross-sectional profile along its length in order to minimize drag on the spoke under crosswind conditions. And alternatively, either the spoke or the tailfin could be tapered in a step-wise manner—rather than a smooth manner—in order to reduce fabrication costs.

Furthermore, wider tires with aggressive tread patterns, designed for maximizing traction rather than minimizing drag, contribute to significant drag in many off-road type vehicles. Such tires often have tread patterns with rectangular profiles, which thus suffer higher sensitivities to drag. These tires can be designed with more aerodynamic tread patterns, with the tread blocks shaped either more in an oval shape than a square or rectangular, or more tapered and streamlined on the leeward sides, thereby maintaining much of the traction of the rectangular profile tread tire. Furthermore, designing the gaps between the tread blocks for streamlined flow of headwinds around these tread blocks, could improve vehicle propulsive efficiencies. Moreover, the tread blocks could be shaped to freely divert some of the headwind to the side of the tire, especially for the upper forward profile section of the tire, rather than simply forcing the air up and over the tire, producing additional turbulence and more drag.

And as has been shown, the addition of minimal upper- and forwardly-oriented fairing and fender assemblies can substantially reduce total drag on the wheel, thereby enhancing the propulsive efficiency of the vehicle. Such shielding devices should see widespread application on a range of different vehicles, from human-powered bicycles to high-speed motorcycles, automobiles, and trucks and trailers. The embodiments shown are poised to contribute not only to improved vehicle propulsive efficiency, but also to the worldwide effort to reduce vehicle fuel consumption—and thereby to conserve valuable energy resources.

While the embodiments shown illustrate application generally to front-wheel assemblies on various vehicles, the embodiments could be similarly applied to the rear or intermediate wheels of any wheeled vehicle or vehicle trailer. And while the embodiments illustrated demonstrate shielding applied primarily to the front-most section of upper wheel assemblies, such shields may be extended to closely cover the entire upper half of wheels, especially where enhanced streamlining is desired and sensitivity to crosswinds is not important, as can often be the case for powered cycles and motor vehicles. Accordingly, the embodiments should not be limited to the specific examples illustrated and described above, but rather to the appended claims and their legal equivalents. 

I claim:
 1. An apparatus for reducing aerodynamic drag-induced resistive forces upon a terrestrial vehicle employing a wheel assembly exposed to headwinds and crosswinds above the level of an axle of the wheel assembly when the vehicle is in forward motion, comprising: a longitudinally tapered structural spoke fastening an outer rim to a central hub of a wheel assembly exposed to headwinds impinging thereon above the level of an axle of said wheel assembly while employed on a vehicle in forward motion; said tapered spoke disposed to reduced drag from a combined headwind and crosswind impinging on a surface of said spoke when said surface is positioned directly above the axle within an uppermost region of said wheel assembly comprising a major upper drag-inducing surface, with said region being located wholly above the level of the axle of said wheel assembly and including primary vehicle-drag inducing wheel surfaces; said tapered spoke having a plurality of different cross-sectional profile shapes spaced along a longitudinal section of the tapered spoke with each said cross-sectional shape varying unidirectionally along the longitudinal section from one to the next adjoining said cross-sectional shape, progressing from a thin aerodynamic cross-sectional profile located proximate to an end of said tapered spoke attached to the rim of said wheel assembly to a substantially circular cross-sectional profile located toward an opposite end of said tapered spoke attached to the central hub of said wheel assembly; said tapered spoke when positioned directly above the axle having the longitudinal section extending from proximate to said tapered spoke end attached to the rim toward said opposite tapered spoke end attached to the central hub a sufficient distance to thereby extend substantially across said region with at least a first portion of the longitudinal section extending downwards from the level of a critical elevation which is generally centered around the primary vehicle-drag inducing wheel surfaces; said tapered spoke when positioned directly above the axle having at least a second portion of the longitudinal section extending above the level of the critical elevation; and said tapered spoke providing reduced drag on said wheel assembly from the combined headwind and crosswind wherein the net drag-induced resistive forces from the combined wind impinging said longitudinal section within said region are reduced and the vehicle propulsive counterforces needed to countervail said net drag-induced resistive forces are reduced and wherein the effective traction of said wheel assembly where contacting against the ground is increased and wherein the net drag-induced resistive forces on said tapered spoke in the most elevated position being applied higher on said wheel assembly near the level of the critical elevation than the countervailing vehicle propulsive counterforces being applied lower in elevation at the axle, and having a substantial mechanical advantage over the countervailing vehicle propulsive counterforces since both the resistive forces and the counterforces are levered in opposition about the same lowermost stationary point of ground contact on said wheel assembly with the moment arms of the resistive forces being substantially longer than the moment arms of the counterforces, a reduction in the net drag-induced resistive force from the varying combined winds impinging on the longitudinal section of the tapered spoke, which when positioned within said region thereabout primary vehicle-drag inducing wheel surfaces has winds with differing effective relative directions and stronger effective headwind speeds impinging lengthwise thereon, is magnified by the mechanical advantage, yielding substantial reductions in overall vehicle drag.
 2. The apparatus of claim 1, further comprising: said tapered spoke is solid; and the spoke circular cross-sectional profile shape having substantially constant shape within each of a series of longitudinal subsections spaced along the longitudinal section.
 3. The apparatus of claim 1, further comprising: said tapered spoke is solid; spoke surfaces within a mid-section along said spoke having a substantially circular cross-sectional profile shape; and the spoke circular cross-sectional profile shape varying substantially smoothly along the longitudinal section.
 4. The apparatus of claim 1, further comprising: said tapered spoke is solid; spoke surfaces within a mid-section along said spoke having a substantially circular cross-sectional profile shape; and the spoke circular cross-sectional profile shape having substantially constant shape within each of a series of longitudinal subsections spaced along the longitudinal section.
 5. The apparatus of claim 1, further comprising: said tapered spoke is solid; spoke surfaces within a mid-section along said spoke having a substantially circular cross-sectional profile shape; and the cross-sectional area of the spoke is substantially constant in area along the longitudinal section.
 6. An apparatus for reducing aerodynamic drag-induced resistive forces upon a terrestrial vehicle employing a wheel assembly exposed to headwinds impinging thereon above the level of an axle of the wheel assembly when the vehicle is in forward motion, comprising: an upper wheel fairing disposed attachably to a nonrotatable structural portion of a frame or a body of a vehicle employing a wheel assembly exposed to headwinds impinging thereon above the level of an axle of said wheel assembly while the vehicle in forward motion; the wheel fairing placed proximally adjacent to a structural wheel surface which includes a major proportion of a primary drag-inducing portion of a major upper drag-inducing surface located wholly above the level of the axle of said wheel assembly, with said drag-inducing portion also being located in a region of said wheel assembly positioned forward of the axle and generally centered both above and below around the level of a critical elevation which is generally centered around the primary vehicle-drag inducing wheel surfaces, with the structural wheel surface including a major proportion of the primary vehicle-drag inducing wheel surfaces; the wheel fairing diverting an oncoming headwind from otherwise impinging upon the structural wheel surface; the structural wheel surface extending downwards and forwards to include the major proportion of said drag-inducing portion while extending anywhere no lower than a minimum level below which placement of the wheel fairing would otherwise cause a net increase in the drag-induced resistive forces upon the vehicle; the structural wheel surface having at least a portion thereof extending above the level of the critical elevation; the wheel fairing surfaces extending no further both upward and downward from the level of the critical elevation and no further both forward and rearward of the structural wheel surface and no further laterally distant apart from the structural wheel surface than which all taken together the net drag induced upon extended surfaces of the wheel fairing would otherwise offset the reduced drag on the wheel and cause a net increase in the drag-induced resistive forces upon the vehicle when the vehicle is operated nominally under null headwind conditions; the wheel fairing surfaces extending no further radially apart from said structural wheel surface equal to ten percent of the diameter of said wheel assembly; the wheel fairing surfaces extending no further laterally apart from said structural wheel surface equal to ten percent of the diameter of said wheel assembly; and the wheel fairing providing substantial wind shielding of the structural wheel surface from the headwind wherein the net drag-induced resistive forces upon the structural wheel surface are reduced and the vehicle propulsive counterforces needed to countervail said net drag-induced resistive forces are reduced and wherein the effective traction of said wheel assembly where contacting against the ground is increased and wherein said wind shielding by the wheel fairing of primary vehicle-drag inducing wheel surfaces, which have stronger effective headwinds otherwise impinging thereon, yielding substantial reductions in overall vehicle drag from the net drag-induced resistive force, which would otherwise be applied higher on said wheel assembly near the level of the critical elevation than the countervailing vehicle propulsive counterforce being applied lower in elevation at the axle and would therefore have a substantial mechanical advantage over the countervailing vehicle propulsive counterforce because both said resistive force and said counterforce would be levered in opposition about the same lowermost stationary point of ground contact on said wheel assembly with the moment arm of said resistive force being substantially longer than the moment arm of said counterforce, being applied instead on the wheel fairing disposably attached to the vehicle frame where a fairing drag force thereon is countervailed through the vehicle frame from a propulsively driven wheeled axle of the vehicle having a proportional propulsive countertorque equivalent to a countervailing propulsive force being transmitted from the wheel assembly and applied to the vehicle frame at the level of the axle which would suffer no mechanical disadvantage over the fairing drag force since both the fairing drag force and the countervailing propulsive force would be in direct opposition at the same level at the axle.
 7. The wheel fairing of claim 6, further comprising: the wheel fairing being limited to extend no further radially apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; and the wheel fairing being limited to extend no further laterally apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly.
 8. The wheel fairing of claim 6, further comprising: the wheel fairing being limited to extend no further radially apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; the wheel fairing being limited to extend no further laterally apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; and the wheel fairing wherein said wheel assembly is disposed on the front wheel of the vehicle.
 9. The wheel fairing of claim 6, further comprising: the wheel fairing wherein the structural wheel surface includes only wheel surfaces positioned within a distance of the critical elevation equal to or less than 15 percent of the diameter of said wheel assembly and wherein the structural wheel surface may extend above or below the critical elevation; the wheel fairing being limited to extend no further radially apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; and the wheel fairing being limited to extend no further laterally apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; and the wheel fairing wherein said wheel assembly is disposed on the front wheel of the vehicle.
 10. An apparatus for optimal minimization of aerodynamic drag-induced resistive forces upon a terrestrial vehicle employing a wheel assembly exposed to headwinds impinging thereon above the level of an axle of the wheel assembly when the vehicle is in forward motion, comprising: a drag-reduction apparatus placed attachably to a vehicle employing a wheel assembly exposed to headwinds impinging thereon above the level of an axle of said wheel assembly while the vehicle in forward motion wherein: the drag is reduced on a major upper drag-inducing surface of said wheel assembly located wholly above the level of an axle of said wheel assembly and including primary vehicle-drag inducing wheel surfaces; the major upper drag-inducing surface extending downwards from the level of a critical elevation which is generally centered around the primary vehicle-drag inducing wheel surfaces to no lower than a minimum level below which an oncoming headwind impinging upon the major upper drag-inducing surface would otherwise cause a net increase in the drag-induced resistive forces upon the vehicle; the major upper drag-inducing surface and having at least a further portion thereof extending above the level of the critical elevation; the net moment of combined drag forces exerted on the major upper drag-inducing surface pivoting about the lowermost stationary point of ground contact on said wheel assembly is reduced; and the drag-reduction apparatus providing reduced drag on the major upper drag-inducing surface from the headwind wherein the net drag-induced resistive forces from the headwind impinging upon the major upper drag-inducing surface are reduced and the vehicle propulsive counterforces needed to countervail said net drag-induced resistive forces are reduced and wherein the effective traction of said wheel assembly where contacting against the ground is increased and wherein the net drag-induced resistive forces from headwinds impinging upon the major upper drag-inducing surface being applied higher on said wheel assembly near the level of the critical elevation than the countervailing vehicle propulsive counterforces being applied lower in elevation at the axle, and having a substantial mechanical advantage over the countervailing vehicle propulsive counterforces since both the resistive forces and the counterforces are levered in opposition about the same lowermost stationary point of ground contact on said wheel assembly with the moment arms of the resistive forces being substantially longer than the moment arms of the counterforces, a reduction in the net drag-induced resistive force from headwinds impinging upon the major upper drag-inducing surface positioned thereabout primary vehicle-drag inducing wheel surfaces, which also have stronger effective headwinds impinging thereon, is magnified by the mechanical advantage, yielding substantial reductions in overall vehicle drag.
 11. The drag-reduction apparatus of claim 10, further comprising: a wind shielding apparatus that is disposed attachably to a nonrotatable structural portion of a frame or a body of the wheeled vehicle wherein the wind shielding apparatus being placed proximally adjacent to a structural wheel surface which includes a major proportion of a primary drag-inducing portion of the major upper drag-inducing surface, with said drag-inducing portion also being located in a region of said wheel assembly positioned forward of the axle and generally centered both above and below around the level of the critical elevation, with the structural wheel surface including a major proportion of the primary vehicle-drag inducing wheel surfaces; the wind shielding apparatus adapted to shield the structural wheel surface from the headwind otherwise impinging thereon; the structural wheel surface extending downwards and forward to include the major proportion of said portion of the major upper drag-inducing wheel surface; the wind shielding apparatus being limited in combined shielding extent both upward and downward from the level of the critical elevation and both forward and rearward of the structural wheel surface and in lateral distance apart from the structural wheel surface no further than which all taken together the net drag induced upon extended surfaces of the wind shielding apparatus would otherwise offset the reduced drag on the wheel and cause a net increase in the drag-induced resistive forces upon the vehicle when the vehicle is operated nominally under null headwind conditions; the wind shielding apparatus being limited to extend no further radially apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus being limited to extend no further laterally apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus wherein the structural wheel surface includes only wheel surfaces positioned within a distance of the critical elevation equal to or less than 15 percent of the diameter of said wheel assembly and wherein the structural wheel surface may extend above or below the critical elevation; the wind shielding apparatus wherein said wheel assembly is disposed on the front wheel of the vehicle; and the wind shielding apparatus providing reduced drag force on the structural wheel surface.
 12. The drag-reduction apparatus of claim 10, further comprising: a wind shielding apparatus that is disposed attachably to a nonrotatable structural portion of a frame or a body of the wheeled vehicle wherein the wind shielding apparatus being placed proximally adjacent to a structural wheel surface which includes a major proportion of a primary drag-inducing portion of the major upper drag-inducing surface, with said drag-inducing portion also being located in a region of said wheel assembly positioned forward of the axle and generally centered both above and below around the level of the critical elevation, with the structural wheel surface including a major proportion of the primary vehicle-drag inducing wheel surfaces; the wind shielding apparatus adapted to shield the structural wheel surface from the headwind otherwise impinging thereon; the structural wheel surface extending downwards and forward to include the major proportion of said portion of the major upper drag-inducing wheel surface; the wind shielding apparatus being limited in combined shielding extent both upward and downward from the level of the critical elevation and both forward and rearward of the structural wheel surface and in lateral distance apart from the structural wheel surface no further than which all taken together the net drag induced upon extended surfaces of the wind shielding apparatus would otherwise offset the reduced drag on the wheel and cause a net increase in the drag-induced resistive forces upon the vehicle when the vehicle is operated nominally under null headwind conditions; the wind shielding apparatus being limited to extend no further radially apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus being limited to extend no further radially apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; the wind shielding apparatus being limited to extend no further laterally apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus being limited to extend no further laterally apart from said structural wheel surface equal to 75 percent of the lateral width of a tire of said wheel assembly; the wind shielding apparatus wherein the structural wheel surface includes only wheel surfaces positioned within a distance of the critical elevation equal to or less than 15 percent of the diameter of said wheel assembly and wherein the structural wheel surface may extend above or below the critical elevation; the wind shielding apparatus wherein said wheel assembly is disposed on the front wheel of the vehicle; and the wind shielding apparatus providing reduced drag force on the structural wheel surface.
 13. The drag-reduction apparatus of claim 10, further comprising: a wind shielding apparatus that is disposed attachably to a nonrotatable structural portion of a frame or a body of the wheeled vehicle wherein the wind shielding apparatus being placed proximally adjacent to a structural wheel surface which includes a major proportion of a primary drag-inducing portion of the major upper drag-inducing surface, with said drag-inducing portion also being located in a region of said wheel assembly positioned forward of the axle and generally centered both above and below around the level of the critical elevation, with the structural wheel surface including a major proportion of the primary vehicle-drag inducing wheel surfaces; the wind shielding apparatus adapted to shield the structural wheel surface from the headwind otherwise impinging thereon; the structural wheel surface extending downwards and forward to include the major proportion of said portion of the major upper drag-inducing wheel surface; the wind shielding apparatus being limited in combined shielding extent both upward and downward from the level of the critical elevation and both forward and rearward of the structural wheel surface and in lateral distance apart from the structural wheel surface no further than which all taken together the net drag induced upon extended surfaces of the wind shielding apparatus would otherwise offset the reduced drag on the wheel and cause a net increase in the drag-induced resistive forces upon the vehicle when the vehicle is operated nominally under null headwind conditions; the wind shielding apparatus being limited to extend no further radially apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus being limited to extend no further radially apart from said structural wheel surface equal to half the lateral width of a tire of said wheel assembly; the wind shielding apparatus being limited to extend no further laterally apart from said structural wheel surface equal to 15 percent of the diameter of said wheel assembly; the wind shielding apparatus being limited to extend no further laterally apart from said structural wheel surface equal to the lateral width of a tire of said wheel assembly; the wind shielding apparatus wherein said wheel assembly is disposed on the front wheel of the vehicle; and the wind shielding apparatus providing reduced drag force on the structural wheel surface.
 14. The drag-reduction apparatus of claim 10, further comprising: a longitudinally tapered structural solid spoke fastening an outer rim to a central hub of said wheel assembly and disposed to reduce drag from the headwind combined with a crosswind impinging on a surface of said spoke when said surface is positioned directly above the axle within an uppermost region of said wheel assembly comprising the major upper drag-inducing surface; said tapered spoke having a plurality of different cross-sectional profile shapes spaced along a longitudinal section of the tapered spoke with each said cross-sectional shape varying unidirectionally along the longitudinal section from one to the next adjoining said cross-sectional shape, progressing from a thin aerodynamic cross-sectional profile located proximate to an end of said tapered spoke attached to the rim of said wheel assembly to a substantially circular cross-sectional profile located toward an opposite end of said tapered spoke attached to the central hub of said wheel assembly; spoke surfaces within a mid-section along said spoke having a substantially circular cross-sectional profile shape; said cross-sectional shapes varying substantially smoothly between contiguous locations spaced along the longitudinal section; said tapered spoke when positioned directly above the axle having the longitudinal section extending from proximate to said tapered spoke end attached to the rim toward said opposite tapered spoke end attached to the central hub a sufficient distance to thereby extend substantially across said region with at least a first portion of the longitudinal section extending downwards from the level of the critical elevation; said tapered spoke when positioned directly above the axle having at least a second portion of the longitudinal section extending above the level of the critical elevation; and said tapered spoke providing reduced drag on said wheel assembly from the headwind wherein the net drag-induced resistive forces from the combined wind impinging said longitudinal section are reduced and wherein the reduced drag on the tapered spoke from the varying combined winds having different effective relative directions and speeds where impinging along the longitudinal section when positioned above the level of the axle thereabouts the primary vehicle-drag inducing wheel surfaces yielding substantial reductions in overall vehicle drag.
 15. The drag-reduction apparatus of claim 10, further comprising: a longitudinally tapered structural solid spoke fastening an outer rim to a central hub of said wheel assembly and disposed to reduce drag from the headwind combined with a crosswind impinging on a surface of said spoke when said surface is positioned directly above the axle within an uppermost region of said wheel assembly comprising the major upper drag-inducing surface; said tapered spoke having a plurality of different cross-sectional profile shapes spaced along a longitudinal section of the tapered spoke with each said cross-sectional shape varying unidirectionally along the longitudinal section from one to the next adjoining said cross-sectional shape, progressing from a thin aerodynamic cross-sectional profile located proximate to an end of said tapered spoke attached to the rim of said wheel assembly to a substantially circular cross-sectional profile located toward an opposite end of said tapered spoke attached to the central hub of said wheel assembly; spoke surfaces within a mid-section along said spoke having a substantially circular cross-sectional profile shape; said cross-sectional shapes substantially constant in area as measured at contiguous locations along the longitudinal section; said tapered spoke when positioned directly above the axle having the longitudinal section extending from proximate to said tapered spoke end attached to the rim toward said opposite tapered spoke end attached to the central hub a sufficient distance to thereby extend substantially across said region with at least a first portion of the longitudinal section extending downwards from the level of the critical elevation; said tapered spoke when positioned directly above the axle having at least a second portion of the longitudinal section extending above the level of the critical elevation; and said tapered spoke providing reduced drag on said wheel assembly from the headwind wherein the net drag-induced resistive forces from the combined wind impinging said longitudinal section are reduced and wherein the reduced drag on the tapered spoke from the varying combined winds having different effective relative directions and speeds where impinging along the longitudinal section when positioned above the level of the axle thereabouts the primary vehicle-drag inducing wheel surfaces yielding substantial reductions in overall vehicle drag.
 16. The drag-reduction apparatus of claim 10, further comprising: a spoke tailfin disposed in longitudinal rotatable attachment to a structural spoke with said structural spoke fastening an outer rim to a central hub of said wheel assembly, wherein said tailfin may swivel freely about the longitudinal axis of said spoke in response to varying winds impinging thereon; said tailfin progressively varies in streamlined shape along the length of said tailfin from having a longer fin-like cross-sectional profile proximate to an end for attachment near the rim of said wheel assembly to having a shorter fin-like cross-sectional profile near an opposite end for attachment toward the central hub of said wheel assembly; said tailfin employed on said spoke disposed to reduced drag from the headwind impinging thereon when said tailfin is positioned directly above the axle in a most elevated position within an uppermost region of said wheel assembly comprising the major upper drag-inducing surface; said tailfin when positioned directly above the axle having at least a portion thereof extending downwards from the level of the critical elevation; to no lower than a minimum level below which the headwind impinging thereon would otherwise cause a net increase in the drag-induced resistive forces upon the vehicle; said tailfin when positioned directly above the axle having at least a further portion thereof extending above the level of the critical elevation; and said tailfin providing reduced drag on said spoke from the headwind wherein when said tailfin is in the most elevated position the net drag-induced resistive forces from the varying combined winds, which have different effective relative directions and speeds where impinging thereon along a length of said spoke, are reduced.
 17. The drag-reduction apparatus of claim 10, further comprising: a tire disposed on said wheel assembly with said tire oriented for minimal drag when said tire rotates forwardly; said tire having tread blocks disposed in a patterned arrangement on said tire; said tread blocks on either side of a centerline of said patterned arrangement positioned symmetrically therein, with the centerline being perpendicular to the axle; a majority of said tread blocks each having a ground-contacting profile of the same general shape; said majority blocks each having a convex smoothly-varying aerodynamic ground-contacting profile shape on a predominately leeward-facing surface; those said majority blocks on either one of said sides of the centerline positioned with the predominately longitudinal clearance there-between those said majority blocks not exceeding the predominately lateral clearance there-between those said majority blocks, where the longitudinal direction is parallel to the centerline; those said majority blocks on either one of said sides of the centerline positioned with said predominately longitudinal clearance there-between those said majority blocks not exceeding half the predominate lateral width of those said majority blocks; those said majority blocks on either one of said sides of the centerline positioned sufficiently far apart with sufficient clearance to permit minimally-restricted air flow from a headwind flowing there-between those said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; those said majority blocks on either one of said sides of the centerline positioned sufficiently close together with minimal clearance to redirect air flow from said headwind there-between those said majority blocks onto trailing leeward surfaces of adjacent said majority blocks in sufficient amount to substantially increase aerodynamic pressure on said trailing leeward surfaces in comparison to the aerodynamic pressure on forwardly-oriented windward surfaces of adjacent said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; said majority blocks providing reduced drag on the major upper drag-inducing surfaces of said majority blocks when positioned in the forward upper quadrant of said wheel assembly; and wherein a reduction in the difference in air pressure between a windward-facing surface of said second majority block and the leeward-facing surface of said second majority block causing a reduction in drag force on said second majority block and wherein the net drag-induced resistive forces upon said wheel assembly from headwinds impinging said majority blocks located thereabout the level of the critical elevation are reduced.
 18. The drag-reduction apparatus of claim 10, further comprising: a tire disposed on said wheel assembly with said tire oriented for minimal drag when said tire rotates forwardly; said tire having tread blocks disposed in a patterned arrangement on said tire; said tread blocks on either side of a centerline of said patterned arrangement positioned symmetrically therein, with the centerline being perpendicular to the axle; a majority of said tread blocks each having a ground-contacting profile of the same general shape; said majority blocks each having a convex smoothly-varying aerodynamic ground-contacting profile shape on a predominately leeward-facing surface; those said majority blocks on either one of said sides of the centerline positioned with the predominately longitudinal clearance there-between those said majority blocks not exceeding the predominately lateral clearance there-between those said majority blocks, where the longitudinal direction is parallel to the centerline; those said majority blocks on either one of said sides of the centerline positioned with said predominately longitudinal clearance there-between those said majority blocks not exceeding half the predominate lateral width of those said majority blocks; those said majority blocks on either one of said sides of the centerline positioned sufficiently far apart with sufficient clearance to permit minimally-restricted air flow from a headwind flowing there-between those said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; those said majority blocks on either one of said sides of the centerline positioned sufficiently close together with minimal clearance to redirect air flow from said headwind there-between those said majority blocks onto trailing leeward surfaces of adjacent said majority blocks in sufficient amount to substantially increase aerodynamic pressure on said trailing leeward surfaces in comparison to the aerodynamic pressure on forwardly-oriented windward surfaces of adjacent said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; said majority blocks comprising a first subset of trailing majority blocks located at least partly rearwardly-offset from a second subset of leading majority blocks when said first and second majority blocks are positioned in the forward upper quadrant of said wheel assembly; said tire having said majority blocks with a said first and a said second majority blocks positioned in the forward upper quadrant of said wheel assembly at the level of the critical elevation; said patterned arrangement of adjacent said majority blocks adapted to divert the headwind flowing there-between from a windward-facing surface of said first trailing majority block toward a leeward-facing surface of said second leading majority block; said majority blocks providing reduced drag on the major upper drag-inducing surfaces of said majority blocks when positioned in the forward upper quadrant of said wheel assembly; and wherein a reduction in the difference in air pressure between a windward-facing surface of said second majority block and the leeward-facing surface of said second majority block causing a reduction in drag force on said second majority block and wherein the net drag-induced resistive forces upon said wheel assembly from headwinds impinging said majority blocks located thereabout the level of the critical elevation are reduced.
 19. The drag-reduction apparatus of claim 10, further comprising: a tire disposed on said wheel assembly with said tire oriented for minimal drag when said tire rotates forwardly; said tire having tread blocks disposed in a patterned arrangement on said tire; said tread blocks on either side of a centerline of said patterned arrangement positioned symmetrically therein, with the centerline being perpendicular to the axle; a majority of said tread blocks each having a ground-contacting profile of the same general shape; said majority blocks each having a convex smoothly-varying aerodynamic ground-contacting profile shape on a predominately leeward-facing surface; those said majority blocks on either one of said sides of the centerline positioned with the predominately longitudinal clearance there-between those said majority blocks not exceeding the predominately lateral clearance there-between those said majority blocks, where the longitudinal direction is parallel to the centerline; those said majority blocks on either one of said sides of the centerline positioned with said predominately longitudinal clearance there-between those said majority blocks not exceeding half the predominate lateral width of those said majority blocks; those said majority blocks on either one of said sides of the centerline positioned sufficiently far apart with sufficient clearance to permit minimally-restricted air flow from a headwind flowing there-between those said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; those said majority blocks on either one of said sides of the centerline positioned sufficiently close together with minimal clearance to redirect air flow from said headwind there-between those said majority blocks onto trailing leeward surfaces of adjacent said majority blocks in sufficient amount to substantially increase aerodynamic pressure on said trailing leeward surfaces in comparison to the aerodynamic pressure on forwardly-oriented windward surfaces of adjacent said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; said majority blocks comprising a first subset of trailing majority blocks located at least partly rearwardly-offset from a second subset of leading majority blocks when said first and second majority blocks are positioned in the forward upper quadrant of said wheel assembly; said tire having said majority blocks with a said first and a said second majority blocks positioned in the forward upper quadrant of said wheel assembly at the level of the critical elevation; said patterned arrangement of adjacent said majority blocks adapted to divert the headwind flowing there-between from a windward-facing surface of said first trailing majority block toward a leeward-facing surface of said second leading majority block; said majority blocks including sharp angular windward-facing surfaces; said majority blocks providing reduced drag on the major upper drag-inducing surfaces of said majority blocks when positioned in the forward upper quadrant of said wheel assembly; and wherein a reduction in the difference in air pressure between a windward-facing surface of said second majority block and the leeward-facing surface of said second majority block causing a reduction in drag force on said second majority block and wherein the net drag-induced resistive forces upon said wheel assembly from headwinds impinging said majority blocks located thereabout the level of the critical elevation are reduced.
 20. The drag-reduction apparatus of claim 10, further comprising: a tire disposed on said wheel assembly with said tire oriented for minimal drag when said tire rotates forwardly; said tire having tread blocks disposed in a patterned arrangement on said tire; said tread blocks on either side of a centerline of said patterned arrangement positioned symmetrically therein, with the centerline being perpendicular to the axle; a majority of said tread blocks each having a ground-contacting profile of the same general shape; said majority blocks each having a convex smoothly-varying aerodynamic ground-contacting profile shape on a predominately leeward-facing surface; those said majority blocks on either one of said sides of the centerline positioned with the predominately longitudinal clearance there-between those said majority blocks not exceeding the predominately lateral clearance there-between those said majority blocks, where the longitudinal direction is parallel to the centerline; those said majority blocks on either one of said sides of the centerline positioned with said predominately longitudinal clearance there-between those said majority blocks not exceeding half the predominate lateral width of those said majority blocks; those said majority blocks on either one of said sides of the centerline positioned sufficiently far apart with sufficient clearance to permit minimally-restricted air flow from a headwind flowing there-between those said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; those said majority blocks on either one of said sides of the centerline positioned sufficiently close together with minimal clearance to redirect air flow from said headwind there-between those said majority blocks onto trailing leeward surfaces of adjacent said majority blocks in sufficient amount to substantially increase aerodynamic pressure on said trailing leeward surfaces in comparison to the aerodynamic pressure on forwardly-oriented windward surfaces of adjacent said majority blocks when said majority blocks are positioned at the level of the critical elevation in the forward upper quadrant of the major upper drag-inducing surface of said wheel assembly; said majority blocks comprising a first subset of trailing majority blocks located at least partly rearwardly-offset from a second subset of leading majority blocks when said first and second majority blocks are positioned in the forward upper quadrant of said wheel assembly; said tire having said majority blocks with a said first and a said second majority blocks positioned in the forward upper quadrant of said wheel assembly at the level of the critical elevation; said patterned arrangement of adjacent said majority blocks adapted to divert the headwind flowing there-between from a windward-facing surface of said first trailing majority block toward a leeward-facing surface of said second leading majority block; said tread blocks including sharp angular windward-facing surfaces in oblique orientation to the axis of said wheel assembly wherein impinging air flow is directed in part laterally and rearwardly toward an exterior side of said tire; said majority blocks providing reduced drag on the major upper drag-inducing surfaces of said majority blocks when positioned in the forward upper quadrant of said wheel assembly; and wherein a reduction in the difference in air pressure between a windward-facing surface of said second majority block and the leeward-facing surface of said second majority block causing a reduction in drag force on said second majority block and wherein the net drag-induced resistive forces upon said wheel assembly from headwinds impinging said majority blocks located thereabout the level of the critical elevation are reduced. 